CR 010130, Attachment A WWW.NASAWATCH.COM SSP 54015 Baseline (DRAFT)
Increment Definition and Requirements Document for Increment 15
International Space Station Program
Baseline
September 2006
National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas SSP 54015 WWW.NASAWATCH.COM SSCN XXXX Attachment A Baseline (DRAFT)
REVISION AND HISTORY PAGE
REV. DESCRIPTION PUB. DATE
- Initial Release (Reference per SSCD XXXXXX, EFF. XX-XX-XX) XX-XX-XX SSP 54015 WWW.NASAWATCH.COM SSCN XXXX Attachment A Baseline (DRAFT)
INTERNATIONAL SPACE STATION PROGRAM
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
CHANGE SHEET
September, 2006
Baseline
Space Station Control Board Directive XXXXXX/(X-X), dated XX-XX-XX. (X)
CHANGE INSTRUCTIONS
SSP 54015, Increment Definition and Requirements Document for Increment 15, has been baselined by the authority of SSCD XXXXXX. All future updates to this document will be identified on this change sheet. SSP 54015 WWW.NASAWATCH.COM SSCN XXXX Attachment A Baseline (DRAFT)
INTERNATIONAL SPACE STATION PROGRAM
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
Baseline (Reference SSCD XXXXXX, dated XX-XX-XX)
LIST OF EFFECTIVE PAGES
September, 2006
The current status of all pages in this document is as shown below: Page Change No. SSCD No. Date SSP 54015 WWW.NASAWATCH.COM SSCN XXXX Attachment A Baseline (DRAFT)
INTERNATIONAL SPACE STATION PROGRAM
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
SEPTEMBER 2006
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PREFACE
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
This document is the Increment Definition and Requirements Document for Increment 15. Official delivery of this document is under control of the Space Station Control Board (SSCB). Any changes or revisions will be jointly agreed to and signed by the National Aeronautics and Space Administration (NASA) and the affected International Partners (IPs).
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NASA/ROSCOSMOS
INTERNATIONAL SPACE STATION PROGRAM
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
SEPTEMBER 2006
Michael T. Suffredini Alexi Krasnov National Aeronautics and Space Roscosmos, Director, Manned Flight Administration Program Manager, International Space Station Program
Date Date
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NASA/CSA
INTERNATIONAL SPACE STATION PROGRAM
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
SEPTEMBER 2006
Michael T. Suffredini Benoit Marcotte National Aeronautics and Space CSA Program Manager Administration Manager, International Space Station Program
Date Date
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NASA/ESA
INTERNATIONAL SPACE STATION PROGRAM
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
SEPTEMBER 2006
Michael T. Suffredini Alan Thirkettle National Aeronautics and Space ESA Program Manager Administration Manager, International Space Station Program
Date Date
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INTERNATIONAL SPACE STATION PROGRAM
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
CONCURRENCE
SEPTEMBER 2006
Concurred by: Valeri Ryumin RSC-E ISS PROGRAM DIRECTOR ORG
SIGNATURE DATE
Developer Concurrence: Nikolai Bryukhanov RSC-E DEPUTY ISS PROGRAM DIRECTOR ORG
SIGNATURE DATE
Developer Concurrence: Igor Khamits RSC-E RUSSIAN SEGMENT INTEGRATION ORG
SIGNATURE DATE
Developer Concurrence: Mikhail Shutikov RSC-E RUSSIAN MODULES MANAGER ORG
SIGNATURE DATE
Developer Concurrence: Marina Sycheva RSC-E PLANNING AND MANIFEST MANAGER ORG
SIGNATURE DATE
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INTERNATIONAL SPACE STATION PROGRAM
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
CONCURRENCE
SEPTEMBER 2006
Developer Concurrence: Iliya Filippov RSC-E VEHICLE INTEGRATED PERFORMANCE RESOURCES ORG REPRESENTATIVE
SIGNATURE DATE
Developer Concurrence: Galina Kaportseva RSC-E PROGRAM MANAGER ORG
SIGNATURE DATE
Developer Concurrence: Natalya Zabolotnaya RSC-E MANIFEST AND CREW PROVISIONING ORG REPRESENTATIVE
Ludmila Chaykina SIGNATURE DATE
Developer Concurrence: RSC-E FLIGHT MECHANICS REPRESENTATIVE ORG
SIGNATURE DATE
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INTERNATIONAL SPACE STATION PROGRAM
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
CONCURRENCE
SEPTEMBER 2006
Prepared by: Nancy Monsees OC BOOK MANAGER ORG
SIGNATURE DATE
Concurred by: Susan Brand OC INCREMENT 15 MANAGER ORG
SIGNATURE DATE
Concurred by: Melissa Gard OC REQUIREMENTS AND INCREMENT INTEGRATION ORG MANAGER
SIGNATURE DATE
Concurred by: Kenneth O. Todd OC MISSION INTEGRATION AND OPERATIONS OFFICE ORG MANAGER
SIGNATURE DATE
MIC DQA: Delegated Representative OH DATA MANAGEMENT ORG
SIGNATURE DATE
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INTERNATIONAL SPACE STATION PROGRAM
INCREMENT DEFINITION AND REQUIREMENTS DOCUMENT FOR INCREMENT 15
LIST OF CHANGES
SEPTEMBER 2006
All changes to paragraphs, tables, and figures in this document are shown below:
SSCB Entry Date Change Paragraph(s)
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TABLE OF CONTENTS
PARAGRAPH PAGE
1.0 INTRODUCTION ...... 1-1 1.1 PURPOSE ...... 1-1 1.2 SCOPE...... 1-1 1.3 PRECEDENCE...... 1-2 1.4 DELEGATION OF AUTHORITY ...... 1-2 1.5 DEVIATION...... 1-2 2.0 DOCUMENTS...... 3 2.1 APPLICABLE DOCUMENTS ...... 3 2.2 REFERENCE DOCUMENTS...... 6 3.0 INCREMENT DEFINITION...... 7 3.1 INCREMENT OVERVIEW...... 7 3.2 INCREMENT FLIGHT SUMMARY ...... 9 3.3 INCREMENT SUMMARY AND OBJECTIVES...... 12 3.4 DEVIATIONS TO THE GENERIC GROUNDRULES, REQUIREMENTS, AND CONSTRAINTS DOCUMENT...... 15 4.0 ON-ORBIT RESOURCE ASSUMPTIONS AND ALLOCATIONS...... 16 4.1 POWER BALANCE AND ALLOCATIONS ...... 16 4.2 CREW TIME ...... 19 4.3 ACCOMMODATIONS ...... 20 4.4
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6.4.5 JETTISON REQUIREMENTS...... 43 6.4.6 GROUND SYSTEMS REQUIREMENTS...... 43 6.5 FLIGHT 13A.1 REQUIREMENTS...... 45 6.5.1
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APPENDIX
A ACRONYMS AND ABBREVIATIONS ...... A-67 B GLOSSARY OF TERMS ...... B-76 C OPEN WORK...... C-82 D TOPOLOGIES ...... D-86 E INCREMENT CONFIGURATIONS...... E-93 F
TABLE
TABLE 3.2-1 INCREMENT FLIGHT SUMMARY
FIGURE
3.1-1 INCREMENT 15 OVERVIEW
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1.0 INTRODUCTION
1.1 PURPOSE
This document provides the assignment of flight dates, resources and accommodations, as well as defines the requirements for Increment 15 in Planning Period 7. Requirements are provided for both joint International Space Station (ISS)/mated vehicle operations and ISS-only continuous operations stages of the increment.
The schedule for products (i.e., documentation, reviews, etc.) that must be developed to support Increment 15 is found in the Common Schedule Database (CSD).
1.2 SCOPE
This document covers Increment 15, beginning with the launch of the ISS-15 Commander (CDR) and Flight Engineer (FE) on Flight 14 Soyuz and ends with their departure on Flight 14 Soyuz. The third ISS crew member, FE2, rotates on the Shuttle flights. At the start of Increment 15, the ISS FE2 (ISS 12A.1 FE) will have been on ISS since Flight 12A.1 in Increment 14. The ISS 13A.1 FE is launched on Flight 13A.1 and replaces the ISS 12A.1 FE. The ISS 13A.1 FE returns on Flight 10A. The ISS 10A FE is launched on Flight 10A and replaces the ISS 13A.1 FE. The ISS 10A FE returns during Increment 16. Note that the Flight
This document defines the capabilities and objectives of Increment 15. This document also controls the following: resource and accommodation allocations between assembly, system, and utilization; requirements and priorities for ISS execution planning; ISS manifest [Increment Definition and Requirements Document for Increment 15, Annex 1: Station Manifest (SSP 54015-14S
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1.3 PRECEDENCE
SSP 54015 will be developed in compliance with the specification documents. Deviations from the specifications are possible only as a result of specific scenarios analysis. If there are any discrepancies between this document and SSP 54100, SSP 54100 takes precedence. If there are any discrepancies between this document, SSP 50110, Multi-Increment Manifest Document, and the Consolidated Operations and Utilization Plan, this document shall take precedence.
The real-time time frame for a flight and its associated stage begins after the applicable Stage Operations Readiness Review (SORR) in accordance with the process in SSP 50200-02, Station Program Implementation Plan (SPIP) Volume 2: Program Planning and Manifesting. The differences between the “as planned” requirements in the IDRD and the “real-time” requirements will be documented in SSP 543XX, Post Increment Evaluation Report for Increment 15
This document should be used in conjunction with SSP 50261-01, Generic Groundrules, Requirements, and Constraints Part 1: Strategic and Tactical Planning. Deviations to SSP 50261-01 for this increment are documented in Section 3.4.
1.4 DELEGATION OF AUTHORITY
The Space Station Control Board (SSCB) has formal control and approval of this document. All changes to this document will be processed in accordance with the procedures as specified in SSP 50123, Configuration Management Handbook.
1.5 DEVIATION
Any request for deviation from this document shall be made to the Space Station Program Control Board (SSPCB) in accordance with the procedures as specified in SSP 41170, Configuration Management Requirements. NASA will maintain this document and process changes per these requirements. IPs should provide any recommended changes to the NASA Mission Integration and Operations Office for processing.
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2.0 DOCUMENTS
2.1 APPLICABLE DOCUMENTS
The following documents include specifications, models, standards, guidelines, handbooks, and other special publications. The documents listed in this paragraph are applicable to the extent specified herein. Inclusion of applicable documents herein does not in any way supersede the order of precedence identified in Paragraph 1.3 of this document.
DOCUMENT TITLE TYPE
SSP 41170 Configuration Management Requirements NASA Internal
SSP 50110 Multi-Increment Manifest Document Multilateral
SSP 50123 Configuration Management Handbook Multilateral
SSP 50200-02 Station Program Implementation Plan, Multilateral Volume 2: Program Planning and Manifesting
SSP 50255 Flight Mechanics - Trajectory Bilateral
SSP 50260 International Space Station Medical Operations Multilateral Requirements Document (ISS MORD)
SSP 50261-01 Generic Groundrules, Requirements, and Multilateral Constraints Part 1: Strategic and Tactical Planning
SSP 50562 ISS Program Off-Nominal Situation Plan Multilateral
SSP 54014 Increment Definition and Requirements Document Multilateral for Increment 14
SSP 54015-14S Increment Definition and Requirements Document Multilateral
SSP 54015-26P Increment Definition and Requirements Document Multilateral
SSP 54015-ATV1 Increment Definition and Requirements Document Multilateral
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SSP 54015-13A.1 Increment Definition and Requirements Document Multilateral
SSP 54015-27P Increment Definition and Requirements Document Multilateral
SSP 54015-10A Increment Definition and Requirements Document Multilateral
SSP 54015-ANX 2 Increment Definition and Requirements Document Multilateral
SSP 54015-ANX 3 Increment Definition and Requirements Document Multilateral
SSP 54015-ANX 4 Increment Definition and Requirements Document Multilateral
SSP 54015-ANX 5 Increment Definition and Requirements Document Multilateral
SSP 54016 Increment Definition and Requirements Document Multilateral
SSP 54100 Increment Definition and Requirements Document Multilateral Flight Program
SSP 543XX Post Increment Evaluation Report: Increment 15 Multilateral
NSTS 21477 International Space Station-10A Mission NASA Internal Integration Plan
NSTS 21506 International Space Station-13A.1 Mission NASA Internal Integration Plan
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NAS15-10110 Contract NAS15-10110 between the National Bilateral Aeronautics and Space Administration of the United States of America and the Russian Space Agency of the Russian Federation for Supplies and Services Relating to MIR-1 and the International Space Station: Phase One and Selected Phase Two Activities
JSC 26557 On-orbit Assembly, Modeling, and Mass NASA Internal Properties Data Book
No Number Consolidated Operations and Utilization Plan Multilateral
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2.2 REFERENCE DOCUMENTS
The following documents contain supplemental information to guide the user in the application of this document. These reference documents may or may not be specifically cited within the text of this document.
DOCUMENT TITLE TYPE
SSP 41000 System Specification for the International Space NASA Internal Station
SSP 41162 Segment Specification for the United States NASA Internal On-Orbit
SSP 41163 Russian Segment Specification Bilateral
SSP 50094 NASA/RSA Joint Specifications Standards Bilateral Document for the ISS Russian Segment
SSP 50129 Interface Requirements Document International Multilateral
SSP 50439 ESA Segment Specification for the Automated Multilateral
SSP 50448 Station Development Test Objectives (SDTO) Multilateral Catalog
SSP 50478 Payload Data Library Requirements Document NASA Internal
SSP 50699-03 USOS Certification Baseline Volume III: Flight Multilateral Attitudes
SSP 54014-13S Increment Definition and Requirements Document Multilateral
SSP 54014-25P Increment Definition and Requirements Document Multilateral
SSP 543XX Post Increment Evaluation Report for Increment Multilateral
NSTS 12820 Joint Shuttle/ISS Flight Rules Volume C Joint NASA Internal Operations
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3.0 INCREMENT DEFINITION
This section defines the Increment 15 objectives. The inclusion of objectives in this document provides ISS Program Office control of major events and emphasis during this time frame.
3.1 INCREMENT OVERVIEW
Figure 3.1-1, Increment 15 Overview, provides a high level graphical overview of the increment. It contains the increment’s duration, when and where vehicles are docked to the ISS, planned crew rotations, the number of ISS crew on ISS, and the number of Shuttle and Soyuz (SZ) visiting crews.
The number of planned United States On-orbit Segment (USOS) and Russian Segment (RS) Extravehicular Activities (EVAs) are also shown in this figure. The two contingency EVAs specified in SSP 50261-01, Section 4.3.2.10, are not shown in this figure.
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Feb 07 Mar 07 Apr 07 May 07 Jun 07 Jul 07 Aug 07 Sep 07 Oct 07 Nov 07
Increments Inc 14 CDR Inc 16 CDR Inc 14 FE Inc 16 FE Inc 15 CDR Inc 15 FE Shows Crew Handover Period ISS 12A.1 FE ISS 13A.1 FE ISS 10A FE RS Elements EVAs RS USOS
Visiting
SM Aft 14S ATV 1
Legend: - Assembly EVA performed by the Shuttle crew - Assembly EVA performed by the ISS crew while Shuttle docked - Assembly EVA performed by the ISS crew - Projected maintenance EVA performed by the Shuttle crew - Projected maintenance EVA performed by the ISS crew while Shutt le docked - Maintenance EVA performed by the ISS crew - Science EVAs by the Shuttle crew - Science EVAs by the ISS crew while Shuttle docked - Science EVAs by the ISS crew - Shuttle objective EVA performed by the Shuttle Crew - Contains science EVA activities *# - Contains Shuttle objective EVA activities - Special Activity
FIGURE 3.1-1 INCREMENT 15 OVERVIEW
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3.2 INCREMENT FLIGHT SUMMARY
Table 3.2-1, Increment Flight Summary, identifies planning data for all flights scheduled to visit the ISS or undock from the ISS during this increment.
The mission duration column lists the planned mission duration of each flight. For Shuttle flights in this column, two numbers are listed: 1. The nominal mission duration. 2. Additional contingency days available to accomplish ISS mission objectives (to cover docking problems, mated operations delays, EVA, etc.. The docked duration column lists the planned docked duration for each flight. Duration calculations are based on the calendar day difference between events.
All planning docking altitudes presented in this document represent average altitudes unless stated otherwise. Altitudes are defined in accordance with SSP 50255, Flight Mechanics - Trajectory.
For those Shuttle missions identified to be performance critical, the docking altitudes are to be maximum apogee altitude limits. ISS Flight Mechanics will coordinate with Shuttle Flight Design at the start of each increment design cycle to identify performance-critical missions. Modifications to the altitude strategy will be made in the final increment product cycle.
All launch dates in Table 3.2-1 are shown in the time standard selected by the launch vehicle organization. Space Shuttle Program dates correspond to the Kennedy Space Center (KSC) time zone. Russian dates correspond to the Decreed Moscow Time (DMT) zone. Automated Transfer Vehicle (ATV) dates correspond to the Kourou time zone.
Soyuz ascent crew size is denoted in the “Launch Vehicle Crew Size” column in Table 3.2-1, using the following convention: x+y, where x=number of Expedition crew members and y=number of Soyuz crew members. Soyuz descent crew size will be identified with a table note when it differs from ascent crew size.
Shuttle ascent crew size is denoted in the “Launch Vehicle Crew Size” column in Table 3.2-1, using the following convention: w+z, where w=number of Shuttle Transportation System (STS) crew members and z=number of Expedition crew members. Shuttle descent crew size will be identified with a table note when it differs from ascent crew size.
Table 3.2-1 provides the official program agreements for ATV1. For working direction, the earliest ATV1 launch and dock dates are May 1 (earliest agreed to opportunity) and May 18 (GGR&C guideline H.2.1), respectively. Based on Progress 27, Flight 10A, and 15 Soyuz vehicle traffic dates in Table 3.2-1 and GGR&C guidelines H.2.14, H.2.15B,
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H.2.17, H.2.19, H.2.12, and H.2.13.B, the latest ATV1 undock date is July 23, 2006. The ATV1 data in Figure 3.1-1 reflects these working dates.
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TABLE 3.2-1 INCREMENT FLIGHT SUMMARY
See the last paragraph of Section 3.2 for ATV1 dock and undock working dates to be used by the increment until agreed to dates have been approved.
ISS Launch Launch Planned Mission Shuttle Planned Docked Planned Flight Vehicle Vehicle Launch Duration Docking Docking Duration Undocking Name Flight Crew Size Date (Days) Altitude Date (Days) Date Name (km/nmi) 13S Soyuz-TMA 2+1 [1] 186 - [1] 184 19 Mar 07
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3.3 INCREMENT SUMMARY AND OBJECTIVES
The increment definitions and primary objectives for assembly, system, and utilization operations are provided in Table 3.3-1, Increment 15 Summary. The Multilateral Crew Operations Panel (MCOP) defines crew assignments and respective agencies.
TABLE 3.3-1 INCREMENT 15 SUMMARY
Increment Start Flight 14S Launch (09 Mar 07)
Increment 15/Total Increment 15/Total ISS 12A.1 FE (103/190)
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• Life Support and Habitation: MAMS, LOCAD-PTS • Space Operations: SPHERES, EarthKAM, MISSE PEC 3 / 4, ALTEA, EMCH, CEO • Space Product Development- MSFC: CGBA-4, CSI-01 • MELFI, MSG, HRF Facility Operations Russian: Reference IDRD Section 6.2.1 and SSP 54015-ANX 5/15 CSA: PMDIS (prep for Shuttle crewmember), TRAC Flight 13A.1 Assembly/System • Install and activate ITS S5 Objectives • Transfer and install ESP-3 • Perform cargo transfers • Perform Flight 10A preparatory tasks • Relocate S5 PVRGF • Relocate CETA carts • Reconfig SASA equipment • Cinch P6 Fwd PVR • Install IBA OSE on S1 • Open the Lab H2 Vent Valve for Regen ECLSS system • Perform Educator Astronaut Activities • Rotate ISS 12A.1 FE with ISS 13A.1 FE Flight 13A.1 Utilization Objectives NASA: Conduct On-orbit research program to support: • HRP-JSC: Journals • Perform Operations to support the following SDBIs and Sorties: • HRP-JSC: Midodrine, Sleep Short, PMZ, Latent Virus • Space Product Development- MSFC: CBTM-02 • Fundamental Space Biology-ARC: SPEGIS • Space Operations: EPO Educator, M-CCM, MAUI, RAMBO Russian: Reference IDRD Section 6.2.1 and SSP 54015-ANX 5/15 CSA: PMDIS Stage 13A.1 Assembly/System • Load and undock 26 Progress Objectives • Launch and Dock 27 Progress • Activate OGS • Load and Undock ATV1 from SM Aft • Perform Flight 10A preparatory tasks • Retract FGB Solar Array • Relocate PMA3 from Node 1 Port to Node 1 Nadir • Jettison Early Ammonia Servicer • Install Integrated Station LAN (ISL) Stage 13A.1 Utilization Objectives • NASA: Perform operations to support: • HRP-JSC: Journals, Sleep Long, SWAB, Nutrition, ANITA, CCISS • Space Operations: SPHERES, Elite-S2, EarthKAM, EMCH, EPO, MISSE PEC 3 / 4, EMCH, CEO • Space Product Development- MSFC: CGBA-4, CSI-02 • Life Support and Habitation: MAMS, SAME, LOCAD-PTS • MELFI, MSG, HRF Facility Operations Russian: Reference IDRD Section 6.2.1 and SSP 54015-ANX 5/15 CSA: PMDIS Stow & Setup
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ESA: EMCS MultiGEN-1 Flight 10A Assembly/System • Install Node 2 Objectives • Relocate P6 from Z1 Truss to P5 • Activate P6 • Perform Flight 1E Preparatory Tasks • Install Node 2 PDGF • Install OBSS IBA on S1 • Rotate ISS 13A.1 FE with ISS 10A FE Flight 10A Utilization Objectives NASA: Conduct On-orbit research program to support: • HRP-JSC: Journals • Space Operations: MISSE PEC 3 / 4 EVA retrieval • Perform Operations to support the following SDBIs and Sorties: • HRP-JSC: Midodrine, Sleep Short, PMZ, Latent Virus, Integrated Immune • Space Operations: MAUI, RAMBO Russian: Reference IDRD Section 6.2.1 and SSP 54015-ANX 5/15 CSA: PMDIS Stage 10A Assembly/System • Prepare for 15 Soyuz arrival Objectives • Prepare for Inc 15 ISS CDR and Inc 15 ISS FE departure on 14 Soyuz • Perform Flight 1E Preparatory Tasks (as time permits) Stage 10A Utilization Objectives NASA: Conduct On-orbit research program to support: • HRP-JSC: HRF Facility, Journals, Nutrition, Sleep Long, SWAB, ANITA, CCISS, Mobility • Life Support and Habitation: LOCAD-PTS, SAME, MAMS • Space Operations: SPHERES, Elite-S2, EarthKAM, EPO, CEO • Space Product Development: CGBA, EMCH • MELFI, MSG, HRF Facility Operations Russian: Reference IDRD Section 6.2.1 and SSP 54015-ANX 5/15 NOTE: [1] Flight
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3.4 DEVIATIONS TO THE GENERIC GROUNDRULES, REQUIREMENTS, AND CONSTRAINTS DOCUMENT
The following deviations to SSP 50261-01 have been identified for Increment 15:
None identified.
Violations to SSP 50261-01 groundrules during Increment 15 if identified, are listed on the Increment 15 Management Team website which can be found at the following Uniform Resource Locator (URL): http://iss-www.jsc.nasa.gov/ss/issapt/mio/Inc_15.htm
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ON-ORBIT RESOURCE assumptions AND ALLOCATIONS
This section defines the allocation of the on-orbit ISS capabilities. Allocations are limited to power, crew time, on-orbit accommodations, communications coverage and datalink rates between system and utilization across the increment. Any non-standard requirements of resources are also provided in Section 4.5. The allocation guidelines are baselined in the SSP 50261-01. All data contained in this section represent operational requirements.
3.5 POWER BALANCE AND ALLOCATIONS
Table 4.1-1, Power Balance and Allocations, summarizes ISS power capability and allocations for each flight/stage in the increment. Allocations are representative, and are based on assumed operational mode and the Flight Attitude Plan included in this table. The Flight Attitude Plan was chosen from the attitude envelopes defined in SSP 50699-03 and is the operational plan to meet the energy balance requirement and optimize power availability for Utilization. This plan does not contain attitudes used for waste-water dumps, proximity operations, stage EVAs, etc. Deviations from planned attitudes, and power transfers will be reviewed by the ISS Program, the Operations community, and all affected parties, and will be documented in their respective increment Flight Rules. All calculations in this table represent power availability while the station is in eclipse.
The solar beta angle ranges and attitude symbols also correspond to those defined in SSP 50699-03.
Table 4.1-1 also shows power transfer in kilowatts (kW) between the RS, Functional Cargo Block (FGB), and USOS for the Flight Attitude Plan specified. All values are from the input side of the American-Russian Converter Units (ARCUs) at their saturation point. Power transfer allocation values are based on Russian core system power deficit. However, due to power architecture design constraints in the RS, numbers are shown in ARCU incremental values. USOS may consider cycling the ARCUs to recover power transfer above allocation if needed, and the RS will be notified in advance when cycling will be executed. Power transfers will be updated to meet minimum system power requirements as needed. A negative transfer power number represents a transfer in the opposite direction. For analysis purposes, the FGB is considered to be separate from the RS.
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TABLE 4.1-1 POWER BALANCE AND ALLOCATIONS (PAGE 1 OF 2)
Flight/ Power Availability Power Flight Attitude Power Transfer Power Margin Stage (kW) Consumption Plan (kW) (kW) Total Capability [4] (kW) Allocation to Allocation to Allocation to Systems [1] Utilization [2][3] Systems [1] INCREMENT 15
USOS L [5] M [5] H [5] L [5] M [5] H [5] L [5] M [5] H [5] L [5] M [5] H [5] L [5] M [5] H [5] [5] [6] [6] [6] [6] R Sz 14S 40.9 42.0 42.0 15.5 15.6 15.6 V V V 8.9 8.9 8.9 16.5 17.5 17.5
S 14S [7] 40.9 42.0 42.0 15.5 15.6 15.6 V V V 7.1 7.1 8.9 18.3 19.3 17.5 S 13A [7] 40.9 42.0 42.0 15.5 15.6 15.6 V V V 7.1 7.1 8.9 18.3 19.3 17.5 S 13A [9] 40.9 42.0 42.0 15.5 15.6 15.6 V V V 7.1 7.1 8.9 18.3 19.3 17.5 S 13A 40.9 42.0 42.0 15.5 15.6 15.6 V V V 7.1 7.1 8.9 18.3 19.3 17.5 [10] F 13A.1 40.9 42.0 N/A [6] 18.7 18.7 N/A V V N/A 7.1 7.1 N/A 15.1 16.2 N/A [9] [6] [6] [6] [6] F 13A.1 41.9 42.0 N/A [5] 23.5 23.5 N/A V V N/A 7.1 7.1 N/A 11.3 11.4 N/A [9] [13] [6] [6] [6] [6] S 13A.1 40.9 42.0 42.0 16.0 16.1 16.1 V V V 7.1 7.1 8.9 17.8 18.8 17.0 [9] S 40.9 42.0 42.0 16.0 16.1 16.1 V V V 7.1 7.1 8.9 17.8 18.8 17.0 13A.1[7] F 10A [8] 42.0 42.0 N/A [6] 21.8 21.8 N/A V V N/A 7.1 7.1 N/A 13.1 13.1 N/A [6] [6] [6] [6] F 10A [8] 61.8 63.0 N/A [6] 22.8 22.8 N/A V V N/A 7.1 7.1 N/A 22.2 22.2 N/A [12] [6] [6] [6] [6] S 10A [8] 61.8 63.0 57.0 19.4 19.5 19.5 V V V 7.1 7.1 8.9 22.9 23.1 23.1 S 10A [7] 61.8 63.0 57.0 19.4 19.5 19.5 V V V 7.1 7.1 8.9 22.9 23.1 23.1
FGB L [5] M [5] H [5] L [5] M [5] H [5] L [5] M [5] H [5] L [5] M [5] H [5] L [5] M [5] H [5] [6] [6] [6] [6] [6] R Sz 14S 0.0 0.0 0.0 1.4 1.4 1.4 V V V -1.7 -1.7 -1.7 0.0 0.0 0.0 S 14S 0.0 0.0 0.0 1.4 1.4 1.4 V V V -1.7 -1.7 -1.7 0.0 0.0 0.0 S 13A [7] 0.0 0.0 0.0 1.4 1.4 1.4 V V V -1.7 -1.7 -1.7 0.0 0.0 0.0 S 13A [9] 0.0 0.0 0.0 1.4 1.4 1.4 V V V -1.7 -1.7 -1.7 0.0 0.0 0.0 S 13A 0.0 0.0 0.0 1.4 1.4 1.4 V V V -1.7 -1.7 -1.7 0.0 0.0 0.0 [10] F 13A.1 0.0 0.0 N/A [6] 1.4 1.4 N/A V V N/A -1.7 -1.7 N/A 0.0 0.0 N/A [9] [6] [6] [6] [6] F 13A.1 0.0 0.0 N/A [6] 1.4 1.4 N/A V V N/A -1.7 -1.7 N/A 0.0 0.0 N/A [9] [13] [6] [6] [6] [6] S 0.0 0.0 0.0 1.4 1.4 1.4 V V V -1.7 -1.7 -1.7 0.0 0.0 0.0 13A.1[9] S 13A.1 0.0 0.0 0.0 1.4 1.4 1.4 V V V -1.7 -1.7 -1.7 0.0 0.0 0.0 [7] F 10A [8] 0.0 0.0 N/A [6] 1.4 1.4 N/A V V N/A -1.7 -1.7 N/A 0.0 0.0 N/A [6] [6] [6] [6] F 10A [8] 0.0 0.0 N/A [6] 1.4 1.4 N/A V V N/A -1.7 -1.7 N/A 0.0 0.0 N/A [12] [6] [6] [6] [6] S 10A [8] 0.0 0.0 0.0 1.4 1.4 1.4 V V V -1.7 -1.7 -1.7 0.0 0.0 0.0 S 10A [7] 0.0 0.0 0.0 1.4 1.4 1.4 V V V -1.7 -1.7 -1.7 0.0 0.0 0.0
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TABLE 4.1-1 POWER BALANCE AND ALLOCATIONS (PAGE 2 OF 2)
Flight/ Power Availability Power Flight Attitude Power Transfer Power Margin Stage (kW) Consumption Plan (kW) (kW) Total Capability [4] (kW) Allocation to Allocation to Allocation to Systems [1] Utilization [2][3] Systems [1] INCREMENT 15
RS L [5] M [5] H [5] L [5] M [5] H [5] L [5] M [5] H [5] L [5] M [5] H [5] L [5] M [5] H [5] [11] [11] [6][11] [6] [6] [6] [6]
R Sz 14S 1.8 1.3 0.4 6.4 6.4 6.4 V V V -7.2 -7.2 -7.2 1.4 0.9 0.0 S 14S 1.8 1.3 0.4 5.1 5.1 5.1 V V V -5.4 -5.4 -7.2 1.2 0.7 1.3 S 13A [7] 1.8 1.3 0.4 5.1 5.1 5.1 V V V -5.4 -5.4 -7.2 1.2 0.7 1.3 S 13A [9] 1.8 1.3 0.4 5.5 5.5 5.5 V V V -5.4 -5.4 -7.2 0.8 0.3 0.9 S 13A 1.8 1.3 0.4 5.1 5.1 5.1 V V V -5.4 -5.4 -7.2 1.2 0.7 1.3 [10] F 13A.1 1.8 1.3 N/A [6] 5.5 5.5 N/A V V N/A -5.4 -5.4 N/A 0.8 0.3 N/A [9] [6] [6] [6] [6] F 13A.1 1.8 1.3 N/A [6] 5.5 5.5 N/A V V N/A -5.4 -5.4 N/A 0.8 0.3 N/A [9] [13] [6] [6] [6] [6] S 1.8 1.3 0.4 5.5 5.5 5.5 V V V -5.4 -5.4 -7.2 0.8 0.3 0.9 13A.1[9] S 13A.1 1.8 1.3 0.4 5.1 5.1 5.1 V V V -5.4 -5.4 -7.2 1.2 0.7 1.3 [7] F 10A [8] 1.8 1.3 N/A [6] 5.5 5.5 N/A V V N/A -5.4 -5.4 N/A 0.8 0.3 N/A [6] [6] [6] [6] F 10A [8] 1.8 1.3 N/A [6] 5.5 5.5 N/A V V N/A -5.4 -5.4 N/A 0.8 0.3 N/A [12] [6] [6] [6] [6] S 10A [8] 1.8 1.3 0.4 5.5 5.5 5.5 V V V -5.4 -5.4 -7.2 0.8 0.3 0.9 S 10A [7] 1.8 1.3 0.4 5.1 5.1 5.1 V V V -5.4 -5.4 -7.2 1.2 0.7 1.3
NOTES: [1] Includes power required for assembly and system tasks. [2] Utilization Allocations to each IP based on: NASA: 100 percent of USOS power Roscosmos: 100 percent of RS power. [3] NASA allocation includes FGB and USOS power. [4] Channel power availability is limited to 10.5 kW (includes BCDU limitation and MBSU losses) [5] For stage operations Low Beta is defined as < 37 degrees, Mid Beta is defined between 37 and 52 degrees, High Beta is defined as > 52 degrees [6] Shuttle mated flight ops are constrained to solar beta angles of less than 60 degrees [7] 1 Progress attached to RSOS [8] 2 Progress attached to RSOS [9] 1 Progress, 1 ATV attached to RSOS [10] 1 ATV attached to RSOS [11] SM arrays are parked in the vertical position; data provided by RSC-E. [12] Post P6 Relocation and Activation [13] Station to Shuttle Power Transfer System (SSPTS) active with 2 PTUs
Legend L Low beta angle range LTA Launch To Activation R Sz Soyuz rotation M Mid beta angle range F Flight V XVV flight attitude H High beta angle range S Stage P XPOP flight attitude
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3.6 CREW TIME
Table 4.2-1, Crew Time Allocations, shows the integrated ISS crew time availability, systems demand, and utilization. The ISS utilization allocation will be managed for allocation to the United States, Russian, European, Japanese, and Canadian utilization programs through the Multilateral Payload Control Board (MPCB). The International Partner utilization crew time allocations will be documented in SSP 54015, IDRD for Increment 15 Annex 5.
TABLE 4.2-1 CREW TIME ALLOCATIONS
Crew Time (hours) Total Total Capability [1] 3213 Systems Requirements [2] 3054
Total Allocation to Utilization [3] [4] 159 Utilization Requirements Margin (+/-) NOTES: [1] Includes only ISS-15 crew duty time available during Independent Operations to perform assembly, system, and utilization activities. Includes one hour per crewmember per Saturday or Sunday. [2] In addition to the crew time allocations for stage operations (assembly and systems tasks), additional NASA and Roscosmos systems activities are scheduled during Soyuz and Shuttle docked timeframes per the GGR&C. [3] Utilization planned by each IP based on: NASA: 50 percent of planned Utilization; Roscosmos: 50 percent of planned Utilization [4] Includes ISS-15 crewmember time allocated during Joint Soyuz and Shuttle missions. Refer to section 6 for average weekly crew time allocations.
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3.7 ACCOMMODATIONS
Table 4.3-1, On-Orbit Accommodation Allocations (Pressurized), shows the pressurized on-orbit accommodation allocations for the increment and when the on-orbit internal configuration changes. The unit of measure is Rack Volume Equivalents (RVEs). Russian accommodations are not shown since they are not allocated to the other Partners.
TABLE 4.3-1 ON-ORBIT ACCOMMODATION ALLOCATIONS (PRESSURIZED) (PAGE 1 OF 2)
Rack Volume Equivalents [1] ISS 15 14S-13A.1 13A.1-10A 10A-15S Total Capability (RVE) 43.7 43.7 51.7 Node 1 4 4 4 Node 2 N/A N/A 8 US Lab 24 24 24 Airlock 4 4 4 FGB 11.7 11.7 11.7 NASA Allocation to System Node 1 4 4 4 Node 2 N/A N/A 8 US Lab [2] 13 13 13 Airlock 4 4 4 FGB 10.9 10.9 10.9 NASA Allocation to Utilization Node 1 0 0 0 Node 2 N/A N/A 0 US Lab [3] 11 11 11 Airlock 0 0 0 FGB 0 0 0 Total Amount subscribed [3] 9+1.5 9+1.5 9+1.5 Remaining available 1.5 [5] 1.5 [5] 1.5 [5]
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TABLE 4.3-1 ON-ORBIT ACCOMMODATION ALLOCATIONS (PRESSURIZED) (PAGE 2 OF 2)
Rack Volume Equivalents [1] ISS 15 14S-13A1 13A.1-10A 10A-15S Roscosmos Allocation 0 0 0 Node 1 0 0 0 Node 2 N/A N/A 0 US Lab 0 0 0 Airlock 0 0 0 FGB [4] 0.8 0.8 0.8 NOTES: [1] RVEs can be equated to rack locations in Node 1, US Lab, Airlock, and Node 2. The FGB has 11.7 m3 of stowage volume before installation of new stowage enclosures, which is approximately equal to 11.7 RVEs. [2] During Increment 15, System will use two of the rack locations (TeSS, OGS) in the US Lab allocated to Utilization for pre-positioning of assembly and maintenance hardware. Thirteen rack locations in the US Lab will be allocated to utilization at AC. [3] Utilization items belonging to the Utilization passive stowage RVE allocation might not be physically stowed in the US Lab. [4] Includes 0.8 m3 for stowage provided by FGB enclosures per January 2003 protocol (Ref. OC-03-003). [5] One unsubscribed RVE is positioned in front of Lab window.
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3.8
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3.9
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3.10 ADDITIONAL RESOURCE REQUIREMENT
Table 4.5-1, Additional Resource Requirement, provides the tactical agreements on using non-standard requirements of on-orbit resources (i.e. consumables: water, Oxygen (O2), Nitrogen (N2), propellant, etc.) that is not specified in Sections 4.1 - 4.4 but whose consumption can result in errors of important on board consumables management if not tracked and recorded.
Table 4.5-1 provides the total amount of a resource needed for a specific increment or stage. When the resource is used on-orbit, the resource may be recovered back into resource or emitted in the ISS environment. If the requirement has a closed-loop system, then, the percentage recovered and emitted is not applicable. The utilization allocations will be documented in SSP 54015, IDRD for Increment 15 Annex 5.
TABLE 4.5-1 ADDITIONAL RESOURCE REQUIREMENT
INCREMENT 15 User [1] Resource Total Amount of Usage
Notes: [1] User is defined as the IP needing the resource usage.
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4.0 ASCENT/DESCENT CARGO ALLOCATIONS AND MANIFEST SUMMARY
Table 5.0-1, Ascent/Descent Allocations and Manifest Summary, contains the cargo delivery and return allocations, and the manifest summary for each flight in the increment. The table includes major cargo to the rack or Orbital Replacement Unit (ORU) level. This table controls program-level allocations. Detailed ISS manifest items are documented in the appropriate SSP 54015-XX. The cargo allocations are for the Partner that provides the transportation vehicle unless stated otherwise.
The allocations are based on the Consolidated Operations and Utilization Plan and then refined based on current capability and ISS requirements. Volume data shown is for pressurized stowage areas only and is listed as rack equivalents for full racks in the Multi-Purpose Logistics Module (MPLM), Middeck Locker Equivalents (MLEs) for stowage on the middeck, and Cargo Transfer Bag Equivalents (CTBEs) for passive stowage in the MPLM and SpaceHab, and RVEs for ATV. Progress and Soyuz data are described in terms of volume (in m3) and mass (in kgs. and lbs).The maintenance allocation includes pre-positioned spares and planned maintenance equipment. It does not include items that are considered urgent need spares. Water transfer listed under allocations represents the transfer target for Shuttle water generated on-orbit that is transferred to the ISS. Water transfer listed under International Partner vehicles is water transported up in the International Partner vehicle.
All allocations need to include packing factor and trash. Each owner is responsible for including packing factor and trash.
Soyuz Transportation Modified Anthropometric (TMA) vehicles provide transportation for the Soyuz crew, Expedition crew rotation and will provide the capability for ISS crew rescue return (up to three). The Soyuz TMA has minimal capability to deliver cargo.
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TABLE 5.0-1 ASCENT/DESCENT ALLOCATIONS AND MANIFEST SUMMARY (PAGE 1 OF 3)
Flight Manifest Item Category Mass (kg/lb) Volume 14S ASCENT Manifest Summary Soyuz-TMA Allocations Dry Cargo Roscosmos
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Rack Tare 548/1028 N/A Accommodation and Outfitting Hardware 868/1910 N/A Total Dry Cargo Capability [9] 1517.8/3339 Planned Dry Cargo Ascent - ESA Planned: 242.8/534 1.4 RVE [8] • Non-Utilization (195 kg/429 lb) • Utilization (100 kg/220 lb) - NASA Planned: 1055/2321 5.7 RVE • Non-Utilization (925 kg/2035 lb) • Utilization (350 kg/771 lb) (See Table 5.0-2) - Unsubscribed 220/484 0 Total 1517/3339 6 RVE [7] 13A.1 ASCENT Manifest Summary
SPACEHAB Single Cargo Module (SHSM) ITS-S5: PVRGF ESP-3: NTA, ATA FSE, BCDU, Pitch/Roll Joint, PFRAM (3)Middeck ISS content Shuttle Integration H/W including SSPTS Allocations Russian 37.21/82.04 4.23 CTBE Maintenance 63.87/140.84 X CTBE - Middeck 5.66/12.48 0.13MLE - SHSM 58.21/128.36 2.38 CTBE Crew Provisions 38.26/84.36 X CTBE - Middeck 0/0 X MLE - SHSM 38.26/84.36 3.96 CTBE Utilization 112.6/248.3 - Middeck (Unpowered) 2.5/5.5 0.2 MLE - Middeck (Powered) 110.1/242.8 5.5 MLE - Spacehab 252.4/556.5 16.2 CTBE
STS O2 for EVA prebreathe (4 EVAs) 7.3/16
O2 transfer to ISS A/L HPGTs 0/0
N2 transfer to ISS A/L HPGTs 22.7/50 (Water transfer to ISS) 387/851 387 liters 9 CWCs – (9 Technical, 0 Potable)
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Maintenance 104.79/231.02 X CTBE - Middeck 0.11/0.25 0.01 MLE - SHSM 104.68/230.77 X Racks 3.87 CTBE Crew Provisions 55/121.25 X CTBE - Middeck 0/0 X MLE - SHSM 55.00/121.25 5.44 CTBE Utilization 362/796 - Middeck (Unpowered) 63.6/140.2 3.3 MLE - Middeck (Powered) 110.1/242.8 5.5 MLE - SHSM 136.3/300.4 5.7CTBE 26P DESCENT Nonrecoverable
STS O2 for EVA prebreathe 5.4/12
O2 transfer to ISS A/L HPGTs
N2 transfer to ISS A/L HPGTs
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Manifest Summary Sidewall Carrier SASAICC: Middeck ISS content, Shuttle Integration H/W Allocations Russian
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Table 5.0-1A, Ascent/On-Orbit/Descent Power Allocation for Utilization (Watts), contains power availability for each flight in the increment.
TABLE 5.0-1A ASCENT/ON-ORBIT/DESCENT POWER ALLOCATION FOR UTILIZATION (WATTS)
Flight Ascent On-Orbit Descent 13A.1 213 213 133 10A
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5.0 REQUIREMENTS
This section defines all of the unique programmatic requirements for the increment’s flight and stage intervals necessary to ensure successful completion of planned assembly, maintenance, operations, and utilization of the ISS during the increment. Generic requirements and constraints are documented in SSP 50261-01.
5.1
5.2 INCREMENT 15 SPECIFIC REQUIREMENTS
This section identifies requirements applicable during Increment 15. Detailed requirements and agreements between ISS Program and the Payload Developers (PDs) for payloads are specified in SSP 54015-ANX5.
6.2.1 Russian Utilization Experiments
Russian science experiments to be conducted during Increment 15 shall consist of the following:
6.2.2 Visiting Crew Utilization Experiments
Visiting crew utilization experiments to be performed for Increment 15 shall consist of the following
6.2.3 Automated Transfer Vehicle-1 specific (ATV1) requirements
6.2.3.1 ATV1 Mission Propellant Requirements
6.2.3.2 ATV 1 is a usable stowage volume while docked to ISS and after initial mandatory transfers there will be periodic unloading and loading as necessary.
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5.3 FLIGHT 14S REQUIREMENTS
This section identifies ISS requirements during Flight 14 Soyuz-TMA.
5.3.1
5.3.2 FLIGHT 14S TASKS (IN DESCENDING PRIORITIZED ORDER)
These tasks, listed in order of ISS Program priority, are to be executed during this flight. The order of execution for these tasks in the nominal plan may vary, depending on timeline efficiencies. The following numbered tasks shall be accomplished for successful completion of this flight. 1. Dock Flight 14 Soyuz-TMA to SM Aft port and perform mandatory crew safety briefing (emergency evacuation walk through) for all crew members, including the visiting crew member. [Intravehicular Activity (IVA)] [Imagery] 2. Rotate Expedition 14 Commander and FE crew members with Expedition 15 Commander and FE crew members, transfer mandatory crew rotation cargo, perform mandatory tasks consisting of Sokol suit checkout and transfer and install Visiting Crew’s seat liner in 13 Soyuz. [IVA] 3. Perform minimum crew handover of 12 hours per rotating crewmember which includes crew safety handover. [IVA] [Robotics] 4. Transfer and stow all delivered and returning cargo to and from Soyuz. [IVA] 5. Undock 13 Soyuz-TMA from FGB Nadir port. [IVA] [Imagery] 6. Transfer Visiting Crew cargo. [IVA] 7. Perform USOS/Russian high priority maintenance activities. [IVA] [Imagery] 8. Perform high priority USOS/Russian medical operations (average of 10 crew hours per week). [IVA] [Imagery] 9. Perform high priority OBT substituting planned SSRMS tasks as OBT when appropriate. [IVA] [Robotics] 10. Conduct visiting crew operations.
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D. Conduct transfer activities. 1) Soyuz Unloading 2) Equipment return E. Conduct Communications. 1) Russian Mission Control Center (Soyuz and ISS) 2) Sessions using Sputnik-Service Module (SM) ham radio. F. Conduct Soyuz system maintenance. G. Conduct Soyuz handover. H. Conduct crew life support activities onboard the ISS. 11. Perform USOS/Russian daily ISS payload status checks as required. [IVA] 12. Perform USOS/Russian ISS payload research operations tasks. [IVA] 13. Perform high priority USOS/Russian Public Affairs Office (PAO) events. [IVA] [Imagery] 14. Perform medium priority USOS/Russian maintenance. [IVA] [Imagery] 15. Perform additional 4 hours per rotating crewmember of ISS crew handover (16 hours per crewmember total). [IVA] 16. Transfer remaining cargo items. [IVA] 17. Perform low priority OBT substituting planned SSRMS tasks as OBT when appropriate. [IVA] [Robotics] 18. Perform remaining USOS/Russian PAO events. [IVA] [Imagery] 19. Perform remaining maintenance. [IVA] [Imagery] 20. Perform SDTO 13004-U, Russian Vehicle Docking/Undocking Loads on ISS, for 13S undocking from FGB Nadir port [ISS Wireless Instrumentation System (IWIS required]. [IVA] [Ground]
5.3.3 ISS/VEHICLE ORBITAL AND CONFIGURATION REQUIREMENTS
5.3.3.1 Flight 14 Soyuz-TMA shall dock at the SM Aft port.
5.3.3.2 Flight 13 Soyuz-TMA shall undock from the FGB Nadir port.
5.3.3.3 The ISS shall be in Control Moment Gyroscope (CMG) control with all thrusters inhibited for the following activities:
None Identified.
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5.3.3.4 The ISS shall be in a free drift configuration with the CMGs not controlling and with all thrusters inhibited for the following activities:
None Identified.
5.3.4 CONTINGENCY REQUIREMENTS
5.3.4.1 Mission Control Center - Houston (MCC-H) and Mission Control Center - Moscow (MCC-M) shall build procedures, contingency timelines, and conduct training for the following non-EVA tasks (The items listed below are for unique tasks or first implementation of new tasks. For contingency tasks not listed below, products/planning are already in place from previous flights/stages, or the ISS Program has determined that resources will not be applied to develop products/planning until the contingency is invoked.): A. USOS and/or RS critical maintenance tasks as follows: None identified.
5.3.5 JETTISON REQUIREMENTS
Planning and product development will be performed to support jettison of the following items during EVA. This will include trajectory analysis to ensure acceptable low risk of recontact with ISS and of damage or injury following re-entry, procedures and training for the crew including worksite identification and desired jettison direction and velocity, and related hazard assessments.
5.3.5.1 Planned Jettison
The following items are planned for jettison during EVA in this flight: A. U.S.: None identified. B. Russian: None identified. 5.3.5.2 Contingency Jettison
The following items may require jettison if they cannot be configured safely to allow vehicle dockings or maneuvers or if their continued operation poses a hazard to the EVA crew. A. U.S.: None identified. B. Russian: None identified.
5.3.6 GROUND SYSTEMS REQUIREMENTS
None identified.
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5.4 FLIGHT 14S UNDOCK TO FLIGHT 13A.1 DOCK REQUIREMENTS (STAGE 14S)
This section identifies requirements applicable from Flight 14 Soyuz-TMA undock to Flight 13A.1 dock, including requirements associated with 14 Soyuz relocation, 25 Progress – M undocking, 26 Progress – M docking and ATV1 docking.
5.4.1
5.4.2 STAGE 14S TASKS (IN DESCENDING PRIORITIZED ORDER)
These tasks, listed in order of ISS Program priority, are to be executed during this stage. The order of execution for these tasks in the nominal plan may vary, depending on timeline efficiencies. The following numbered tasks, which include 2 Station-based Orlan EVAs, shall be accomplished for successful completion of this interval. 1. Perform high priority USOS/Russian maintenance and Shuttle Launch Commit Criteria (LCC) for the next flight. [IVA] [Imagery] 2. Complete 25 Progress-M loading of trash and undock from the Docking Compartment (DC)-1 Nadir port. [IVA] [Imagery] 3. Dock 26 Progress-M to DC-1 Nadir port and perform cargo/propellant transfer. [IVA] [Imagery] 4. Perform 14S relocation from SM Aft to FGB Nadir. [IVA] [Imagery] 5. Perform high priority U.S./Russian medical operations (average of 10 crew hours per week). [IVA] [Imagery] 6. Perform high priority OBT (average of 4 crew hours per week) substituting planned SSRMS tasks as OBT when appropriate. [IVA] [Robotics] 7. Perform USOS software CSCI upgrades: A. Transition from Command and Control (CCS) R4 to CCS R6. B. Transition from Portable Computer System (PCS) R9 to PCS R10. C. Transition from Internal Systems (INT) R2 to INT R3. 8. Perform Orlan-based EVAs #18 & #19 for SMDP installation. (SMDP stowage platform needs to be moved prior to PMA3 relocation.) [EVA] A. Transfer SMDP stowage platform from the USOS and stow on the RS. B. Install SMDPs to final configuration. 9. Perform checkout and preparatory tasks for Flight 13A.1. [IVA] A. Position MT/SSRMS at WS #1 (PDGF 1) for Flight 13A.1 joint operations.
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B. Perform SSRMS pre-launch checkout at MSS WS #1. [Robotics] C. Perform Shuttle Tile Photography during Shuttle approach. [Imagery] D. Perform Shuttle Tile Photography preparation. [Imagery] E. Unstow and configure Joint Airlock. F. Complete 13A.1 Pre-pack and transfer tag-up. G. Configure and checkout EVA equipment. H. Complete Flight Plan and EVA timeline reviews. I. Perform tool preparation. 10. Complete ingressing PMA-3 in preparation for relocation (required before PMA-3 relocation). [IVA] A. Destow PMA-3 cargo. B. Replace the Node 1 Port NPRV with IMV cap. C. Replace Early Communication Antenna plate with hatch window. D. Install modified hatch MMOD/thermal cover. E. Install CBCS target/beam. F. Remove and dispose of the Early Comm Groundstrap. 11. Complete IVA installation of OGS 12. Perform ATV1 Flight Demonstration Program as follows (TDRS required): [IVA] A. Install ATV Control Panel, Simvol display unit and ATV Proximity Communication Equipment (PCE) in SM. B. Verify ATV PCE to Ground signal (required 5 days prior to ATV1 launch). C. Prepare two USOS cameras to visually monitor the approach of the ATV from a distance of 1 km until arrival at point S3. D. Demonstration Mission Rendezvous Day 1 – verify Escape commands issued by ATV-CC after approach to point S2. E. Demonstration Mission Rendezvous Day 2 - verify Hold, Resume and Retreat commands after S3 issued by ATV-CC, and Retreat and Escape commands issued by the ISS crew after ATV retreat to point S4. This activity requires visual crew monitoring and crew commanding of the ATV. 13. Dock ATV1 to SM aft port. [IVA] [Imagery] A. Demonstration Mission Rendezvous Day 3 - verify nominal automated docking of ATV1 to ISS. This activity requires visual crew monitoring of the ATV rendezvous and docking activity.
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B. Perform SDTO 13007-U, Automated Transfer Vehicle (ATV) Docking/Undocking Loads on ISS, for ATV docking (IWIS Required).
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29. Install low priority FGB enclosures (Zones 5, 10, 12, 16,19, 21, 23b, 30A, 30b, 31, 36, 40b, 42A, 48) delivered on ATV1. [IVA] [Imagery] 30. Perform SDTO 13005-U, ISS structural Life Validation and Extension, for ISS alone reboost (if reboost is performed). (IWIS required.) [Ground] [IVA] [Imagery] 31. Perform SDTO 13005-U, ISS Structural Life Validation and Extension, for dedicated IVA input (IWIS required). [IVA] [Imagery] [Ground] 32. Perform SDTO 13004-U, Russian Vehicle Docking/Undocking Loads on ISS, for 25 Progress Undocking. (IWIS required.) [IVA] [Ground] 33. Perform SDTO 13004-U, Russian Vehicle Docking/Undocking Loads on ISS, for 26 Progress Docking. (IWIS required.) [IVA] [Ground] 34. Perform SDTO 13004-U, Russian Vehicle Docking/Undocking Loads on ISS, for 14S relocation. [IVA] [Ground] 35. Perform SDTO 13005-U ISS Structural Life Validation and Extension for 13A.1 Orbiter docking. (IWIS required for either 13A or 13A.1 docking.) [IVA] [Ground]
5.4.3 ISS/VEHICLE ORBITAL AND CONFIGURATION REQUIREMENTS
5.4.3.1 The 25 Progress-M shall undock from the DC 1 Nadir port.
5.4.3.2 The 26 Progress-M shall dock to the DC 1 Nadir port.
5.4.3.3 The 14 Soyuz-TMA shall relocate from the SM Aft port to the FGB Nadir port.
5.4.3.4 The ISS shall be in CMG control without ISS thrusters firing for the following activities:
None identified.
5.4.3.5 The ISS shall be in free drift configuration with the CMGs not controlling and without ISS thrusters firing for the following activities: A. For ATV1 Docking –from docking contact until docking interface latch closure. 5.4.3.6 The ISS ATV1 docking attitude shall be LVLH (0,0,0).
5.4.3.7 The ISS shall be in ISS thrusters mode for the following activities: A. ATV1 approach and docking starting 5 hours prior to planned docking.
5.4.3.8 ATV1 Docking Constraints. A. The USOS P4 solar arrays must be configured to avoid RGPS interference during ATV1 rendezvous and docking from the start of SARJ positioning prior to arrival at point S-1/2 until mechanical capture.
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The specific USOS and RS solar array and radiator positions are as follows:
o 1. The SARJ shall be feathered at 0 starting prior to arrival at S-1/2 to avoid RGPS interference. 2. The SARJ must be locked prior to docking. 3. The 2A BGA must be feathered at 90 deg and the 3A BGA must be feathered at 270 deg for the time the SARJ is at 0 deg. The 2/3A BGA must be locked prior to docking. 4. The 4A/1A BGA must be feathered from S3 departure until docking. 5. The FGB arrays should be retracted or feathered if not retracted. 6. The Service Module (SM) arrays shall be positioned at 65 degrees
5.4.3.9 PMA-3 pressurization restricted to occur in +XVV at β > +30 degrees while at Node 1 Port location without heaters connected.
5.4.4 CONTINGENCY REQUIREMENTS
1.1.1.1 MCC-H and MCC-M shall build procedures, contingency timelines, and conduct training to allow the crew to perform the following non-EVA tasks (The items listed below are for unique tasks or first implementation of new tasks. For contingency tasks not listed below, products/planning are already in place from previous flights/stages, or the ISS Program has determined that resources will not be applied to develop products/planning until the contingency is invoked.): A. USOS and/or RS critical maintenance tasks as follows:
None identified. B. Complete critical unfinished Flight 14 Soyuz assembly tasks as follows:
None identified. C. Remove/replace critical spares as follows:
None identified. D. Complete critical unfinished Flight ATV1 tasks as follows: 1. Calculation of ATV1 cargo mass and center of gravity in the event of a contingency requiring the rapid closure of the ATV1 hatch and subsequent departure of the ATV1 from the ISS.
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E. The ISS shall accommodate an extended period of free drift for up to 110 minutes after ATV1 capture.
5.4.4.2 MCC-H and MCC-M shall build task specific procedures, contingency timelines, and conduct training to a high level sufficient to meet the following objectives:
• Identify task specific technical and safety issues.
• Identify on-board equipment required to perform the task.
• Determine the scope of effort required to prepare for the specific configurations, locations, and environmental conditions for the EVA.
• Provide the crew with the proper skill set required to perform the tasks given the on-board proficiency training assets available.
The readiness of these tasks will be based upon the generic development of the task procedures and timelines to a level that can be validated against a set of criteria. For contingency tasks not listed below, products/planning are already in place from previous flights/stages, or the ISS Program has determined that resources will not be applied to develop products/planning and the feasibility to perform those tasks on this flight/increment will be undetermined until the contingency is invoked. A. USOS and/or RS critical maintenance tasks as follows:
6. NH3 Leak Repair (FLAP, Fluid Leak Indicator (FLI))
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2. Deploy S4 SAW. 3. Thermal condition, recondition, and charging of Channel 1A and 3A batteries within 8 days after launch. 4. Verify 1A and 3A SAW positioning capability to support docking and undocking operations for visiting vehicles. 5. Reconfigure P6 for survival power and retract P6 starboard (Channel 2B) SAW. C. Remove/replace critical spares as follows:
None identified.
5.4.5 JETTISON REQUIREMENTS
Planning and product development will be performed to support jettison of the following items during EVA. This will include trajectory analysis to ensure acceptable low risk of recontact with ISS and of damage or injury following re-entry, procedures and training for the crew including worksite identification and desired jettison direction and velocity, and related hazard assessments.
5.4.5.1 Planned Jettison
The following items are planned for jettison during EVA in this stage: A. U.S.: None identified. B. Russian: None identified.
5.4.5.2 Contingency Jettison
The following items may require jettison if they cannot be configured safely to allow vehicle dockings or maneuvers or if their continued operation poses a hazard to the EVA crew. A. U.S.: None identified. B. Russian: None identified.
5.4.6 GROUND SYSTEMS REQUIREMENTS
5.4.6.1 Docking of ATV1 must be planned to occur over Russian ground stations.
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5.4.6.2
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5.5 FLIGHT 13A.1 REQUIREMENTS
This section identifies ISS requirements during Flight 13A.1. Detailed requirements and agreements between the ISS Program and the Space Shuttle Program are specified in NSTS 21506, International Space Station-13A.1 Mission Integration Plan.
5.5.1
5.5.2 FLIGHT 13A.1 TASKS (IN DESCENDING PRIORITIZED ORDER)
These tasks, listed in order of ISS Program priority, are to be executed during this flight. The order of execution for these tasks in the nominal plan may vary, depending on timeline efficiencies. The following numbered tasks, which include 3 Station-based EVAs, with 2 to be performed by the Shuttle crew and 1 to be performed by 1Station crew and 1 Orbiter crew, shall be accomplished for successful completion of this flight. The content for an additional planned EVA is included should a mission duration extension be approved following verification of SSPTS. 1. Inspect Orbiter Reinforced Carbon-Carbon (RCC) using the Shuttle Remote Manipulator System (SRMS) and downlink data. [IVA] [Imagery] [Robotics] 2. Inspect Orbiter tile. [IVA] [Imagery] [Robotics] 3. Dock Shuttle Flight 13A.1 to PMA-2 port and perform mandatory safety briefing for all crew members. [IVA] [Imagery] 4. Rotate ISS 12A.1 FE with ISS 13A.1 FE, transfer mandatory crew rotation cargo per Flight 13A.1 TPL
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8. Relocate S5 PVRGF from launch location to keel location on S5 using SSRMS (required to avoid interference with the S4 solar array rotation and 15A MT translation). [EVA] [Robotics] [Imagery] 9. Perform minimum crew handover of 12 hours per rotating crewmember, which includes crew safety handover. [IVA] 10. Perform Port S-band communications system upgrade. [IVA] [Imagery] A. Relocate the MT/SSRMS to WS4/MBS PDGF #2. [Ground] B. Retract the P6 Photovoltaic Thermal Control System (PVTCS) forward Photovoltaic Radiator (PVR). [Ground] C. Relocate S-band Antenna Sub-Assembly (SASA) from P6 to P1 using SSRMS. [Robotics] [EVA] D. Install the new S-band Transponder and Baseband Signal Processor (BSP) to P1. [EVA] E. Activate the new S-band System. [Ground] 11. Deploy the third External Stowage Platform (ESP-3) with the ATA FSE, 3 empty PFRAMs, Nitrogen Tank Assembly (NTA), SSRMS Roll/Pitch Joint, and Battery Charger/Discharger Unit (BCDU) ORUs from the payload bay and stow it on the P3 Truss Structure using SSRMS and SRMS. [IVA] [Robotics] [Imagery] 12. Relocate 2 Crew and Equipment Translation Aid (CETA) carts to Starboard for P6 relocation using SSRMS. [EVA] [Robotics] 13. Transfer the Inspection Boom Assembly (IBA) Orbital Support Equipment (OSE) to the station and install it on the 2 S1 Zenith Trunnions using SSRMS. [EVA][Robotics][Imagery] 14. Retrieve the P6 Transponder . [EVA] 15. Cinch the P6 PVTCS forward PVR. [EVA] 16. Transfer remaining cargo items per Flight 13A.1 TPL in Appendix I
17. Transfer required N2 from Orbiter to the ISS Airlock (A/L) High Pressure Gas Tanks (HPGTs). [IVA] 18. The following tasks (in priority order) are deemed to fit within the existing EVA timelines; however, may be deferred if the EVA is behind schedule. The EVA will not be extended to complete these tasks. [EVA] [Imagery]
A. Open the H2 vent on the U.S. Lab for Regenerative (Regen) Environmental Control and Life Support System (ECLSS). [EVA] B. Remove and replace S02B-D Remote Power Control Module (RPCM) for Control Moment Gryro (CMG) 2.
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C. Patch Panel reconfiguration for S02B-D RPCM. D. Install External Wireless Instrumentation System (EWIS) antennas (2) on U.S. Lab. E. Route Integrated Station Local Area Network (LAN) (ISL) Cable from Node 1 to FGB (and complete connection if RS cable installed). 19. Perform daily activities to support payloads(included cases where Shuttle crew also performs payloads on the ISS). [IVA] 20. Perform USOS/Russian ISS payload research operations tasks. [IVA] A. Latent Virus B. PMZ C. Sleep Short D. Midodrine E. SPEGIS F. CBTM-02 G. EPO Educator H. M-CCM I. Journals J. PMDIS K. RAMBO L. MAUI 21. Perform imagery survey of the ISS exterior during Orbiter flyaround after undock. [IVA] [Imagery] 22. Perform Program-approved EVA get-ahead tasks. The following EVA get ahead tasks (in priority order) do not fit in the existing EVA timelines; however, the EVA team will be trained and ready to perform should the opportunity arise. EVA/MOD has the flexibility to select the tasks to be completed based on efficiencies gained in performing the already scheduled required tasks. [EVA] [Imagery] [Robotics] A. Jettison EAS using SSRMS (get ahead for Stage 13A.1).
B. Transfer NH3 from Early Ammonia Servicer (EAS) to S1 Ammonia Tank Assembly (ATA) using SSRMS. C. Connect S5 to S4 umbilicals (get ahead for 15A). D. Remove S5 to S6 RTAS Launch Locks (get ahead for 15A). E. Open the S5 RTAS Capture Latch Assembly (get ahead for 15A).
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23. Reboost the ISS with the Orbiter to no more than 185 nmi average orbital altitude
25. Transfer required O2 from Orbiter to the ISS A/L HPGTs. [IVA] 26. Perform SDTO 13005-U, ISS Structural Life Validation and extension, during S5 installation. [Ground] [Imagery] 27. Perform SDTO 13005-U, ISS Structural Life Validation and Extension, during Shuttle mated ISS Reboost (IWIS required) (only if crew time available). [IVA] [Ground] [Imagery] 28. Perform SDTO 13005-U, ISS Structural Life Validation and Extension, during 13A.1 Orbiter Undocking. [Ground]
5.5.3 ISS/VEHICLE ORBITAL AND CONFIGURATION REQUIREMENTS
5.5.3.1 The maximum rendezvous, altitude for Flight 13A.1 shall be 343 km (185 nmi)
5.5.3.2 The Orbiter shall dock at Pressurized Mating Adapter (PMA)-2.
5.5.3.3 The ISS with Shuttle docked shall be in Control Moment Gyroscope (CMG) control without ISS thrusters firing as well as the Shuttle Reaction Control System (RCS) inhibited for the following activities: A. P6 PVTCS Radiator contingency retraction (15 minutes). B. Various EVA manual override tasks. C. SRMS unberthing of ITS S5, handoff to SSRMS, and SSRMS berthing of ITS S5 to ITS S4. 5.5.3.4 The ISS with Shuttle docked shall be in a free drift configuration with the CMGs not controlling, Shuttle RCS inhibited and without ISS thrusters firing for the following activities: None identified.
5.5.3.5 The Space Station Remote Manipulator System (SSRMS) shall be located on the Mobile Servicer (MRS) Base system (MBS)/MT at worksite #1 (PDGF 1) at the beginning of Flight 13A.1.
5.5.3.6 Solar Array Position For Critical Operations: A. During S5 installation, S4 solar arrays shall be fixed at a SARJ angle of 180 degrees and BGA angles of 180 degrees for Channel 1A and 270 for Channel 3A.
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5.5.4 CONTINGENCY REQUIREMENTS
5.5.4.1 Mission Control Center - Houston (MCC-H) and Mission Control Center - Moscow (MCC-M) shall build procedures, contingency timelines, and conduct training for the following non-EVA tasks (The items listed below are for unique tasks or first implementation of new tasks. For contingency tasks not listed below, products/planning are already in place from previous flights/stages, or the ISS Program has determined that resources will not be applied to develop products/planning until the contingency is invoked.): A. USOS and/or RS critical maintenance tasks as follows:
None identified. B. Contingency Orbiter separation from the ISS and re-rendezvous.
5.5.4.2 MCC-H and MCC-M shall build procedures, contingency timelines, and provide pre-flight training for the EVA tasks to sufficient maturity to provide for the EVA response times designated. Examples below are not in prioritized order, but are to show what type of activities could be included. A. Class 1: All procedures, timelines and training are developed and certified to support an EVA response within 24 hours. 1. EVA installation of S5. 2. EVA installation of ESP-3. 3. Contingency power cable routing for stranded MT. B. Class 2: For contingencies occurring during the docked time frame an EVA response is available on a subsequent EVA based on re-prioritization of the mission tasks. Published procedures and timelines are developed, but may require real time updates to match the flight specific failure. None identified. C. Class 3: For contingencies related to first flights hardware that are not time critical, skeleton EVA procedures will be developed preflight to support a Class 3 EVA. The EVA response time can be greater than two weeks and can be deferred to the stage or next available mission. The ISS Program has determined that additional resources will not be applied to further refine the training and integrated planning until the failure occurs. Subsequent flight listings for these hardware items will be contained in the Generic Groundrules, Requirements, and Constraints (GGR&C). None identified.
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5.5.5 JETTISON REQUIREMENTS
Planning and product development will be performed to support jettison of the following items during EVA. This will include trajectory analysis to ensure acceptable low risk of recontact with ISS and of damage or injury following re-entry, procedures and training for the crew including worksite identification and desired jettison direction and velocity, and related hazard assessments.
5.5.5.1 Planned Jettison
The following items are planned for jettison during EVA in this flight: A. U.S.: Early Ammonia Servicer (if 4th EVA occurs) B. Russian: None identified. 5.5.5.2 Contingency Jettison
The following items may require jettison if they cannot be configured safely to allow vehicle dockings or maneuvers or if their continued operation poses a hazard to the EVA crew. A. U.S.: None identified. B. Russian: None identified.
5.5.6 GROUND SYSTEMS REQUIREMENTS
A. Ground Support is required to operate SDMS, IWIS and EWIS for SDTO: 13005-U. B. Ground support is highly desired to operate SAMS-II, MAMS and Russian ALO sensors for SDTO: 13005-U. SAMS and MAMS availability will be assessed real time.
5.5.7 ISS REQUIREMENTS ON SHUTTLE DURING NON-DOCKED TIME FRAME
A. CBTM-02 B. EPO (Educator) C. Latent Virus D. MAUI E. Midodrine F. PMZ G. Sleep Short H. M-CCM
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I. MERLIN
5.6 FLIGHT 13A.1 UNDOCK TO FLIGHT 10A DOCK REQUIREMENTS (STAGE 13A.1)
This section identifies requirements applicable from Flight 13A.1 undock to Flight 10A dock, including requirements associated with 26 Progress-M undocking and 27 Progress – M docking and ATV1 undocking.
5.6.1
5.6.2 STAGE 13A.1 TASKS (IN DESCENDING PRIORITIZED ORDER)
These tasks, listed in order of ISS Program priority, are to be executed during this stage. The order of execution for these tasks in the nominal plan may vary, depending on timeline efficiencies. The following numbered tasks, which include 1 Station-based EMU EVA, shall be accomplished for successful completion of this interval. 1. Perform high priority USOS/Russian maintenance and Shuttle LCC for the next flight. [IVA] [Imagery] 2. Complete 26 Progress-M loading of trash and undock from the Docking Compartment (DC)-1 Nadir port. [IVA] [Imagery] 3. Dock 27 Progress-M to DC-1 Nadir port and perform cargo/propellant transfer. [IVA] [Imagery] 4. Perform high priority U.S./Russian medical operations (average of 10 crew hours per week). [IVA] [Imagery] 5. Perform high priority OBT (average of 4 crew hours per week) substituting planned SSRMS tasks as OBT when appropriate. [IVA] [Robotics] 6. Relocate PMA-3 from Node 1 Port CBM to Node 1 Nadir CBM using SSRMS (required before U.S. Stage EVA and Flight 10A). [IVA] [Robotics] A. Perform CBM proficiency training prior to PMA3 relocation. [IVA] 7. Perform FGB solar array retraction (required before Flight 10A).
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9. Complete ATV1 loading of trash and undock from SM Aft port.
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17. Perform medium-priority USOS/Russian payloads operations (average of
5.6.3 ISS/VEHICLE ORBITAL AND CONFIGURATION REQUIREMENTS
5.6.3.1 The 26 Progress-M shall undock from the DC 1 Nadir port.
5.6.3.2 The 27 Progress-M shall dock to the DC 1 Nadir port.
5.6.3.3 The PMA-3 shall relocate from the Node 1 Port CBM to the Node 1 Nadir CBM using SSRMS.
5.6.3.4 The ISS shall be in CMG control without ISS thrusters firing for the following activities: None identified.
5.6.3.5 The ISS shall be in free drift configuration with the CMGs not controlling and without ISS thrusters firing for the following activities:
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A. ISS shall mode to free drift before physical separation of ATV1. The free drift time should be sufficient for the MCC-M assessment of the mode execution; ATV1 commanding of hooks opening and hooks opening, but not exceed 7 minutes and 10 seconds. 5.6.3.6 The ATV1 shall undock from the SM Aft port.
5.6.3.7 The ISS attitude for ATV1 undocking shall be LVLH (0,0,0).
5.6.3.8 The USOS solar arrays must be feathered to
5.6.4 CONTINGENCY REQUIREMENTS
5.6.4.1 MCC-H and MCC-M shall build procedures, contingency timelines, and conduct training to allow the crew to perform the following non-EVA tasks (The items listed below are for unique tasks or first implementation of new tasks. For contingency tasks not listed below, products/planning are already in place from previous flights/stages, or the ISS Program has determined that resources will not be applied to develop products/planning until the contingency is invoked.): A. USOS and/or RS critical maintenance tasks as follows:
None identified. B. Complete critical unfinished Flight 13A.1 assembly tasks as follows: None identified. C. Remove/replace critical spares as follows:
None identified.
5.6.4.2 MCC-H and MCC-M shall build task specific procedures, contingency timelines, and conduct training to a high level sufficient to meet the following objectives:
• Identify task specific technical and safety issues.
• Identify on-board equipment required to perform the task.
• Determine the scope of effort required to prepare for the specific configurations, locations, and environmental conditions for the EVA.
• Provide the crew with the proper skill set required to perform the tasks given the on-board proficiency training assets available.
The readiness of these tasks will be based upon the generic development of the task procedures and timelines to a level that can be validated against a set of criteria. For contingency tasks not listed below, products/planning are already in place from previous flights/stages, or the ISS Program has determined that resources will not be applied to
-54 SSP 54015 WWW.NASAWATCH.COMWWW.NASAWATCH.COM SSCN XXXX Attachment A Baseline (DRAFT) develop products/planning and the feasibility to perform those tasks on this flight/increment will be undetermined until the contingency is invoked. A. USOS and/or RS critical maintenance tasks as follows:
The tasks listed in Paragraph 6.4.4.2.A. are still applicable. B. Complete critical unfinished Flight 13A.1 assembly tasks as follows: 1. Install IBA OSE on S1 Zenith Trunnions. 2. Relocate 2 CETA Carts. 3. Retract and Cinch P6 PVTCS Forward PVR C. Contingency EVA for manual FGB SA retraction. D. Remove/replace critical spares as follows:
None identified.
5.6.5 JETTISON REQUIREMENTS
Planning and product development will be performed to support jettison of the following items during EVA. This will include trajectory analysis to ensure acceptable low risk of recontact with ISS and of damage or injury following re-entry, procedures and training for the crew including worksite identification and desired jettison direction and velocity, and related hazard assessments.
5.6.5.1 Planned Jettison
The following items are planned for jettison during EVA in this stage: A. U.S.:
• EAS B. Russian: None identified.
5.6.5.2 Contingency Jettison
The following items may require jettison if they cannot be configured safely to allow vehicle dockings or maneuvers or if their continued operation poses a hazard to the EVA crew. A. U.S.:
• PVR radiator
5.6.6 GROUND SYSTEMS REQUIREMENTS
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A. Ground Support is required to operate SDMS, IWIS and EWIS for SDTO 13004-U. B. Ground support is highly desired to operate SAMS-II, MAMS and Russian ALO sensors for SDTO 13004-U. C. Ground support is required to perform SSRMS/MBS prelaunch checkout.
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FLIGHT 10a requirements This section identifies ISS requirements during Flight 10A. Detailed requirements and agreements between the ISS Program and the Space Shuttle Program are specified in NSTS 21477, International Space Station-10A Mission Integration Plan.
5.6.7
5.6.8 FLIGHT 10A TASKS (IN DESCENDING PRIORITIZED ORDER)
These tasks, listed in order of ISS Program priority, are to be executed during this flight. The order of execution for these tasks in the nominal plan may vary, depending on timeline efficiencies. The following numbered tasks, which include 3 Station-based EVAs, with all to be performed by the Shuttle crew, shall be accomplished for successful completion of this flight. 1. Dock Shuttle Flight 10A to PMA-2 port and perform mandatory crew safety briefing for all crew members. [IVA] [Imagery] 2. Install Node 2 to Node 1 Port CBM using SSRMS and activate Node 2 shell heaters. [EVA] [Robotics] [Imagery] [IVA] 3. Rotate ISS 13A.1 FE crew member with ISS 10A FE crew member, transfer mandatory crew rotation equipment per 10A TPL
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D. Connect P5 / P6 utility tray power umbilicals, 1553 command and data buses, and fluid cables E. Configure MBSU jumpers to support P6 start-up on P5 9. Transfer remaining cargo items per Flight 10A TPL
13. Transfer required N2 from the Orbiter to the ISS Airlock HPGTs
14. Transfer required O2 from the Orbiter to the ISS Airlock HPGTs
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B. Install Node 2 external outfitting hardware including the installation of Node 2 handrails (up to 11), and Worksite Inter Faces (WIFs) (up to 3) using SSRMS. [Robotics] [Imagery] C. Release Node 2 zenith Active Common Berthing Mechanism (ACBM) petal restraints and remove up to 4 Node 2 radial hatch latch pins using SSRMS. [Robotics] [Imagery] 21. Perform USOS/Russian ISS payload research operations tasks. [IVA] A. Integrated Immune – SD B. Integrated Immune – LD C. Journals D. Latent Virus E. PMZ F. Sleep Short G. Midodrine H. PMDIS 22. Reboost the ISS with the Orbiter to no more than
23. Reinstall Laboratory (Lab) forward ACBM controller hardware, disconnect O2/N2 lines between Lab and PMA-2, install PMA-2 CBCS target and install US Lab forward outer hatch window hyzod cover (Required prior to final US Lab forward hatch closure and PMA-2 relocation). [IVA] 24. Perform imagery survey of the ISS exterior during Orbiter fly around after undock. [IVA] [Imagery] 25. Perform an additional 4 hours per rotating crewmember of ISS crew handover (16 hours per crew member total). [IVA] 26. Reboost the ISS with the Orbiter to
5.6.9 ISS/VEHICLE ORBITAL AND CONFIGURATION REQUIREMENTS
5.6.9.1 The maximum rendezvous altitude for Flight 10A shall be 325.6 km (185 nmi).
5.6.9.2 The Orbiter shall dock at Pressurized Mating Adapter (PMA)-2.
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5.6.9.3 During P6 removal from Z1, the ISS Ku-Band Antenna shall be fixed at an Elevation of +120 degrees and a Cross Elevation of +65 degrees to allow for clearance between the SSRMS and the antenna.
5.6.9.4 P6 will be placed in an overnight parked position on the SRMS after removal from the Z1 Truss and positioned to maintain the passive thermal requirements.
5.6.9.5 The mated vehicles shall meet the following constraints to mated vehicle attitude control
5.6.9.6 The ISS with Shuttle docked shall be in Control Moment Gyroscope (CMG) control without ISS thrusters firing as well as the Shuttle Reaction Control System (RCS) inhibited for the following activities: A. Unberthing Node 2 from Payload Bay, SSRMS manipulation of Node 2 (i.e., SSRMS in Motion), and berthing Node 2 to Node 1. B. During SRMS and/or SSRMS operations involving P6/Z1 RTAS release, P6 removal, P6 maneuvers, and P6 berthing to P5 until capture and secure with at least three of four bolts. CMG control is not required during overnight park. C. During P6 SAW or PVR retract and deploy or during S1 radiator deploy
5.6.9.7 The ISS with Shuttle docked shall be in a free drift configuration with the CMGs not controlling, Shuttle RCS inhibited and without ISS thrusters firing for the following activities: None identified. 5.6.9.8 Solar Array Position for Critical Operations A. P4 solar arrays shall be feathered and fixed at a SARJ angle of 112.5 degrees and at BGA angles of 50 degrees for channel 4A and 300 degrees for channel 2A while the Orbiter is within a distance of 182.88 m (600 ft) of the ISS for Orbiter approach and docking. B. S4 solar arrays shall be feathered and fixed at a SARJ angle of
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E. S4 solar arrays shall be feathered and fixed at a SARJ angle of
5.6.10 CONTINGENCY REQUIREMENTS
5.6.10.1 Mission Control Center - Houston (MCC-H) and Mission Control Center - Moscow (MCC-M) shall build procedures, contingency timelines, and conduct training for the following non-EVA tasks (The items listed below are for unique tasks or first implementation of new tasks. For contingency tasks not listed below, products/planning are already in place from previous flights/stages, or the ISS Program has determined that resources will not be applied to develop products/planning until the contingency is invoked.): A. USOS and/or RS critical maintenance tasks as follows: None identified. B. Contingency Orbiter separation from the ISS and re-rendezvous. 5.6.10.2 MCC-H and MCC-M shall build procedures, contingency timelines, and provide pre-flight training for the EVA tasks to sufficient maturity to provide for the EVA response times designated. Examples below are not in prioritized order, but are to show what type of activities could be included. A. Class 1: All procedures, timelines and training are developed and certified to support an EVA response within 24 hours. 1. Manually override the radiator deploy/retract motor. B. Class 2: For contingencies occurring during the docked time frame an EVA response is available on a subsequent EVA based on re-prioritization of the mission tasks. Published procedures and timelines are developed, but may require real time updates to match the flight specific failure. 1. Contingency Node 2 CBM berthing. 2. Manually release Node 2 from SSRMS. 3. Manually release and then jettison a radiator. 4. Open Payload Release Latch Assembly (PRLA) 5. Contingency CBM berthing 6. Manually deploy and retract the P6 solar Array wings
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7. Using PRDs to bring the P5/P6 truss segments together in the event of gapping due to SSAS capture latch failure 8. Complete RTAS mating using EVA contingency bolts 9. EVA release of P6 Grapple fixture for failed SRMS end effector 10. EVA Release of SSRMS Latching End Effector (LEE) from P6 Grapple fixture 11. Manually deploy or retract the P6 PVR 12. Re-winch and re-cinch of P6 PVR 13. Re-spool Solar Array Tension/Guide Wires 14. EVA Assisted Deployment of P6 SAWs 15. Manually override the Beta Gimbal anti-rotation latch 16. Perform SARJ DLA Back-off 17. Remove and replace P6 PVR PFCS 18. Remove and replace P6 PV DDC 19. Position any P6 BGA to the SAW orientation to support docking/undocking loads if SAWs already deployed 20. Remove and replace ECU on any P6 module 21. Remove and replace DCSU on P6 22. Install and after restart remove, RACU Restart Cables prior to P6 relocation 23. Orbiter TPS inspection/repair 24. Manually release SSRMS from Node 2 FRGF 25. Manually release and jettison PVR radiator
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5.6.11 JETTISON REQUIREMENTS
Planning and product development will be performed to support jettison of the following items during EVA. This will include trajectory analysis to ensure acceptable low risk of recontact with ISS and of damage or injury following re-entry, procedures and training for the crew including worksite identification and desired jettison direction and velocity, and related hazard assessments.
5.6.11.1 Planned Jettison
The following items are planned for jettison during EVA in this flight: A. U.S.: None identified. B. Russian: None identified. 5.6.11.2 Contingency Jettison
The following items may require jettison if they cannot be configured safely to allow vehicle dockings or maneuvers or if their continued operation poses a hazard to the EVA crew. A. U.S.:
• P6 SAW or PV Radiator
5.6.12 GROUND SYSTEMS REQUIREMENTS
A. Cycle Node 2 heaters while Node 2 is berthed to Node 1.
5.6.13 ISS REQUIREMENTS ON SHUTTLE DURING NON-DOCKED TIME FRAME
A. Integrated Immune B. Latent Virus C. MAUI D. Midodrine E. PMZ F. Sleep Short
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5.7 FLIGHT 10A UNDOCK TO FLIGHT 15S DOCK REQUIREMENTS (STAGE 10A)
This section identifies requirements applicable from Flight 10A undock to Flight 15 Soyuz-TMA dock, including requirements associated with ATV undocking.
5.7.1
5.7.2 STAGE 10A TASKS (IN DESCENDING PRIORITIZED ORDER)
These tasks, listed in order of ISS Program priority, are to be executed during this stage. The order of execution for these tasks in the nominal plan may vary, depending on timeline efficiencies. The following numbered tasks, which include no Station-based EVAs, shall be accomplished for successful completion of this interval. 1. Perform high priority USOS/Russian maintenance and Shuttle LCC for the next flight. [IVA] [Imagery] 2. Perform preparation for Expedition 15 CDR and FE rotation on Soyuz 15. [IVA] 3. Perform high priority U.S./Russian medical operations (average of 10 crew hours/week). [IVA] [Imagery] 4. Perform high priority OBT (average of 4 crew hours per week) substituting planned SSRMS tasks as OBT when appropriate. [IVA] [Robotics] 5. Perform checkout and preparation tasks for Flight 15 Soyuz-TMA arrival and Flight 14 Soyuz-TMA return. [IVA] A. Complete pre-pack and transfer tag-up. B. Perform training and preparation for joint operations, which includes performing Soyuz on-orbit vehicle training/familiarization training for Soyuz 14 crew return. C. Complete Flight Plan reviews. D. Perform tool preparation. 6. Perform high priority USOS/Russian payload operations (average of 6.4 crew hours per week). [IVA] 7. Perform high priority USOS/Russian PAO events (average 2.5 crew hours per week). [IVA] [Imagery] 8. Perform medium priority USOS/Russian maintenance (average of 21.7 crew hours per week). [IVA] [Imagery] 9. Perform medium priority USOS/Russian payloads operations (if crew time permits). [IVA] 10. Reboost ISS with Progress as required. [Ground]
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11. Perform low priority OBT substituting planned SSRMS tasks as OBT when appropriate. [IVA] [Robotics] 12. Perform remaining USOS/Russian PAO events. [IVA] [Imagery] 13. Perform remaining maintenance. [IVA] [Imagery] 14. Perform remaining USOS/Russian payload operations. [IVA] 15. Perform SDTO 13005-U, ISS Structural Life Validation and Extension, for ISS alone reboost (IWIS required). [IVA] [Imagery] [Ground] 16. Perform SDTO 13004-U, Russian Vehicle Docking/Undocking Loads on ISS, for 15 Soyuz docking to SM Aft port. (IWIS required) [IVA] [Ground]
5.7.3 ISS/VEHICLE ORBITAL AND CONFIGURATION REQUIREMENTS
5.7.3.1 The ISS shall be in CMG control without ISS thrusters firing for the following activities:
None identified.
5.7.3.2 The ISS shall be in free drift configuration with the CMGs not controlling and without ISS thrusters firing for the following activities:
None identified.
5.7.4 CONTINGENCY REQUIREMENTS
5.7.4.1 MCC-H and MCC-M shall build procedures, contingency timelines, and conduct training to allow the crew to perform the following non-EVA tasks (The items listed below are for unique tasks or first implementation of new tasks. For contingency tasks not listed below, products/planning are already in place from previous flights/stages, or the ISS Program has determined that resources will not be applied to develop products/planning until the contingency is invoked.): A. USOS and/or RS critical maintenance tasks as follows: None identified. B. Complete critical unfinished Flight 10A assembly tasks as follows: None identified. C. Remove/replace critical spares as follows: None identified. 5.7.4.2 MCC-H and MCC-M shall build task specific procedures, contingency timelines, and conduct training to a high level sufficient to meet the following objectives:
• Identify task specific technical and safety issues.
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• Identify on-board equipment required to perform the task.
• Determine the scope of effort required to prepare for the specific configurations, locations, and environmental conditions for the EVA.
• Provide the crew with the proper skill set required to perform the tasks given the on-board proficiency training assets available.
The readiness of these tasks will be based upon the generic development of the task procedures and timelines to a level that can be validated against a set of criteria. For contingency tasks not listed below, products/planning are already in place from previous flights/stages, or the ISS Program has determined that resources will not be applied to develop products/planning and the feasibility to perform those tasks on this flight/increment will be undetermined until the contingency is invoked. A. USOS and/or RS critical maintenance tasks as follows:
5.7.5 JETTISON REQUIREMENTS
Planning and product development will be performed to support jettison of the following items during EVA. This will include trajectory analysis to ensure acceptable low risk of recontact with ISS and of damage or injury following re-entry, procedures and training for the crew including worksite identification and desired jettison direction and velocity, and related hazard assessments.
5.7.5.1 Planned Jettison
The following items are planned for jettison during EVA in this stage: A. U.S.: None identified. B. Russian: None identified. 5.7.5.2 Contingency Jettison
The following items may require jettison if they cannot be configured safely to allow vehicle dockings or maneuvers or if their continued operation poses a hazard to the EVA crew. A. U.S.: None identified. B. Russian: None identified.
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5.7.6 GROUND SYSTEMS REQUIREMENTS
A. Cycle Node 2 heaters while Node 2 is berthed to Node 1
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Appendix a
Acronyms and abbreviations
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APPENDIX A - ACRONYMS AND ABBREVIATIONS
AC Assembly Complete ACP Automated Transfer Vehicle (ATV) Control Panel Aft At the back of a craft A/L Airlock ALO Optical Linear Accelerometers ANITA Analyzing Interferometer for Ambient Air ANX Annex APFR Articulating Portable Foot Restraint APPC Arm Pitch Plane Change ARCU American-to-Russian Converter Unit ARS Air Revitalization System ATA Ammonia Tank Assembly ATV Automated Transfer Vehicle BCDU Battery Charge/Discharge Unit BGA Beta Gimbal Assembly BITE Built-In Test Equipment BSP Baseband Signal Processor CBCS Centerline Berthing Camera System CBM Common Berthing Mechanism CBTM Commercial Biomedical Testing Module CCAA Common Cabin Air Assembly CCISS Cardiovascular and Cerebrovascular Control on Return from ISS CCS Command and Control System CDR Commander CGBA Commercial Generic Bioprocessing Apparatus CETA Crew and Equipment Translation Aid CHeCS Crew Health Care System CLA Camera and Light Assembly CLPA Camera Light Pan Tilt Assembly CMG Control Moment Gyroscope CoFR Certification of Flight Readiness Comm Communication CR Change Request CSA Canadian Space Agency CSD Common Schedule Database CTB Cargo Transfer Bag CTBE Cargo Transfer Bag Equivalent DC Docking Compartment DCSU Direct Current Switching Unit DDCU-E Direct Current-to-Direct Current Converter Unit - External deg degree DLA Drive Lock Assembly
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DMT Decreed Moscow Time DQA Document Quality Assurance DTO Development Test Objective EAS Early Ammonia Servicer ECLSS Environmental Control and Life Support System ECU Electronics Control Unit EDD Extended Data Dump EDMS Electronic Document Management System EMCH Elastic Memory Composite Hinge EMU Extravehicular Mobility Unit EPO Education Payload Operations ER EXPRESS Rack ESA European Space Agency ESP External Stowage Platform EVA Extravehicular Activity EWIS External Wireless Instrumentation System EXPRESS EXpedite the PRocessing of Experiments to the Space Station EXT External F Flight FE Flight Engineer FEL First Element Launch FGB Functional Cargo Block FHRC Flex Hose Rotary Coupler FLAP Fluid Line Anchor Patch FLI Fluid Line Indicator FMA Force/Moment Accommodation FMS Force Moment Sensor FP Flight Program FRGF Flight Releasable Grapple Fixture FSE Flight Support Equipment ft feet
GGR&C Generic Groundrules, Requirements, and Constraints
H2 Hydrogen H2O Water HPGT High Pressure Gas Tank HRF Human Research Facility H/W Hardware I- Increment minus IBA Inspection Boom Assembly ICC Integrated Cargo Carrier IDRD Increment Definition and Requirements Document IEA Integrated Equipment Assembly
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IELK Individual Equipment Liner Kit IFHX Interface Heat Exchanger IMS Inventory Management System IMV Intra-Module Valve INT Internal IP International Partner ISL Integrated Station LAN ISPR International Standard Payload Rack ISS International Space Station ISS International Space Station ISS MORD International Space Station Medical Operations Requirements Documents ITS Integrated Truss Segment IVA Intravehicular Activity IWIS ISS Wireless Instrumentation System JAXA Japan Aerospace Exploration Agency JCS Joint Control S/W JSC Johnson Space Center kg kilogram km kilometer KSC Kennedy Space Center KURS (English transliteration) Automatic Rendezvous and Docking System kW kilowatt L Launch L- Launch minus Lab Laboratory LAN Local Area Network lb pound LCC Launch Commit Criteria LD Long Duration LEE Latching End Effector LOCAD-PTS Lab-On-a-Chip Applications Development - Portable Test System LOS Loss of Signal LTA Launch To Activation LVLH Local Vertical Local Horizontal M Modified m meter M-CCM Myofibers-Cell Culture Module m3 cubic meter MAMS Microgravity Acceleration Measurement System MAUI Maui Analysis of Upper Atmospheric Injections Mbps Megabits-per-second
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MBS MRS Base System MBSU Main Bus Switching Unit MCC Mission Control Center MCC-H Mission Control Center - Houston MCC-M Mission Control Center - Moscow MCOP Multilateral Crew Operations Panel MDM Multiplexer/Demultiplexer MDSF Manipulator Development and Simulation Facility MELFI Minus Eighty Degree Laboratory Freezer for ISS MIC Mission Integration Contract MIR Mission Integration Review MISSE Materials International Space Station Experiment MLE Middeck Locker Equivalent MMOD Micrometeoroid Orbital Debris MOD Mission Operations Directorate MPLM Multi-Purpose Logistics Module MRS Mobile Remote Servicer MRTAS Modified Rocketdyne Truss Attachment System MSG Microgravity Science Glovebox MSS Mobile Servicing System MT Mobile Transporter N Nadir N/A Not Applicable N2 Nitrogen NASA National Aeronautics and Space Administration NDD Normal Data Dump NET No Earlier Than NH3 Ammonia nmi nautical mile NPRV Negative Pressure Relief Valve NSTS National Space Transportation System
O2 Oxygen OBSS Orbiter Boom Sensor System OBT Onboard Training OCA Orbiter Communication Adapter OCR On-orbit Checkout Requirement OGS Oxygen Generating System ONS Off-Nominal Situation Ops Operations ORG Organization ORU Orbital Replacement Unit OSE Orbital Support Equipment OV Orbiter Vehicle P Progress
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P Port P/L Payload PAO Public Affairs Office PCE Proximity Communication Equipment PCS Portable Computer System PD Payload Developer PDA Personal Digital Assistant PDGF Payload Data Grapple Fixture PEC Passive Experiment Container PFCS Pump Flow Control Subassembly PICB Program Integration Control Board PLB Payload Bay PM Pump Module PMA Pressurized Mating Adapter PMDIS Perceptual Motor Deficits in Space PMZ Promethazine PRD Payload Retention Device PRLA Payload Retention Latch Assembly PTU Pan/Tilt Unit PV Photovoltaic PVCU Photovoltaic Controller Unit PVR Photovoltaic Radiator PVRGF Photovoltaic Radiator Grapple Fixture PVTCS Photovoltaic Thermal Control System PuFF Pulmonary Function in Flight RAMBO RAM Burn Observations RCS Reaction Control System R Russian R Sz Soyuz Rotation R&R Remove and Replace rack loc rack location RACU Russian-to-American Converter Unit RAMBO RAM Burn Observations RBVM Radiator Beam Valve Module RCC Reinforced Carbon-Carbon RCS Reaction Control System Ref Reference RGPS Relative Global Positioning System ROBoT Robotic On-Board Trainer RPCM Remote Power Control Module RS Russian Segment RSA Russian Space Agency RSC-E Rocket Space Corporation - Energia RSP Resupply Stowage Platform RSR Resupply Stowage Rack
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RTAS Rocketdyne Truss Attachment System RVE Rack Volume Equivalent S Starboard SA Solar Array SAMS-II Space Acceleration Measurement System - II SARJ Solar Alpha Rotary Joint SASA S-Band Antenna Sub-Assembly SAW Solar Array Wing SD Short Duration SDBI Short Duration Bioastronautics Investigation SDMS Structural Dynamic Measurement System SDTO Station Development Test Objective SE Subelement SFU Squibb Firing Unit SM Service Module SMDP Service Module Debris Panels SORR Stage Operations Readiness Review SPEGIS S. pneumoniae Expression of Genes in Space SPHERES Synchronized Position Hold, Engage, Reorient, Experimental Satellites SPIP Station Program Implementation Plan SRMS Shuttle Remote Manipulator System SSAS Segment-to-Segment Attach System SSC Station Support Computer SSCB Space Station Control Board SSCD Space Station Change Directive SSP Space Shuttle Program SSPCB Space Station Program Control Board SSPTS Station/Shuttle Power Transfer System SSRMS Space Station Remote Manipulator System SSU Sequential Shunt Unit STS Shuttle Transportation System Sz Soyuz TBD To Be Determined TBR To Be Resolved TCS Thermal Control System TDRS Tracking and Data Relay Satellite TeSS Temporary Sleep Station TMA Transportation Modified Anthropometric TPL Transfer Priority List TPS Thermal Protection System TRAC Test of Reaction and Adaptation Capability
Unpressurized Cargo Carriers Attachment System
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URL Uniform Resource Locator U.S. United States U.S. Lab United States Laboratory USOS United States On-orbit Segment V Velocity Vector VSSA Video Stanchion Support Assembly WETA Wireless Video System External Transceiver Assembly WIF Worksite Interface WS Workstation XPOP X-Axis Perpendicular to Orbital Plane XVV X-Axis into Velocity Vector Z Zenith ZSR Zero-gravity Stowage Rack
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APPENDIX B
GLOSSARY OF TERMS
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APPENDIX B - GLOSSARY OF TERMS
ACCOMMODATIONS Launch vehicles or ISS physical locations where utilization or system items are stowed or installed. The following specific types of accommodations are recognized (the unit of measure of the accommodation is shown in parentheses): A. Rack locations (number) B. MLEs C. CTBEs D. Pressurized volume (RVE) E. Unpressurized volume (cubic feet) F. Truss attach points (number) G. Experiment Module Exposed Facility attach points (number) H. Experiment Logistics Module Exposed Section attach points (number)
ALLOCATION The portioning of resources and accommodations to the ISS users. Total ISS resources and accommodations are allocated between system and utilization. Utilization resources and accommodations are allocated between IPs.
ASSEMBLY PHASE Refers to the time period starting with First Element Launch (FEL) and ending with the landing of the last flight in the assembly sequence.
CARGO CARRIER Element of a transportation vehicle that provides capability to carry cargo.
CHECKOUT To ensure that the rack performs its intended functions with respect to data, power, Thermal Control System (TCS), etc.
CONSOLIDATED OPERATIONS AND UTILIZATION PLAN The strategic document that defines the system and utilization activities planned for the ISS. On a planning period basis, it establishes the amount of resources and accommodations allocated to and subscribed by system and each International Partner for utilization, and reflects the planned amounts of supporting services from other Programs that are available and subscribed. The Consolidated Operations and Utilization Plan also provides specific direction and guidance to tactical planning regarding Consolidated Operations and Utilization Plan implementation.
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CONTINGENCY EXTRAVEHICULAR ACTIVITY An unplanned EVA required to support the safe return of the vehicle and crew and/or restore critical systems/functions.
CREW DAYS IN SPACE The time period from launch of a crew rotation vehicle to landing of the vehicle which returns that crew.
CREW DAYS ON THE ISS The time period from docking of a crew rotation vehicle to undock of the vehicle which returns that crew.
EXECUTION PLANNING The planning that occurs 18 months before the start of an increment through real-time operations.
FLIGHT For Shuttle flights, the term “Flight” refers to the sequence of events that takes place between the lift-off and landing of the Shuttle. For permanent Russian Elements flights, the term refers to the sequence of events that takes place between the lift-off of the element through completion of docking to the ISS. For replaceable IP Element flights, the term refers to the sequence of events that take place between lift-off and entry/landing of the element.
HARD COMMIT Amount of resources allocated to utilization based on specified ISS Program system capabilities.
INCREMENT (Also known as Expedition.) A specific time period which combines different operations such as assembly, scientific research, testing, logistics, maintenance, and other ISS system and utilization operations. The initial unmanned timeframe and subsequently, the timeframe of each crew expedition. During the assembly phase, an increment is defined as a period supporting crew rotation. The duration of an increment is the time period from the launch of a designated Expedition crew to the undocking of the return vehicle for that Expedition crew.
INSTALL Complete the structural attachment and, if applicable, connect utilities.
INTEGRATED TRUSS SEGMENT An un-pressurized structural element of the ISS that includes ground-installed electrical, thermal, communications, command, and data components. Examples are Zenith (Z)1 and Starboard (S)0.
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INTERNATIONAL PARTNER Denotes the international space agencies that are jointly involved in the development of the ISS. These agencies include the Canadian Space Agency (CSA), European Space Agency (ESA), NASA, Japan Aerospace Exploration Agency (JAXA), and Federal Space Agency (Roscosmos).
JETTISON The intentional manual release of an object during an EVA such that the object safely separates from ISS and eventually re-enters through earth's atmosphere. Jettisons may be planned, to achieve waste disposal or scientific objectives, or in response to a contingency, such as inability to install or safely stow or return an item.
KU-BAND 15.250 to 17.250 Gigahertz
LAUNCH VEHICLE A Booster vehicle that delivers the transportation vehicle from the launch pad to an insertion orbit in low earth orbit (Proton, Soyuz, Ariane 5, or H2 for example).
NONRECOVERABLE CARGO Cargo that is designated as cargo that will either be destroyed upon reentry or when it is returned to Earth (e.g., Shuttle/ISS trash).
OBJECTIVES High-level goals that do not specify any particular activity. For an IDRD, each increment will have objectives. During assembly, the main system objectives are building, activating, and supporting the ISS. Examples of utilization objectives during assembly are installing and activating research facility racks, and performing research operations.
PLANNING PERIOD Approximately one calendar year of ISS activity. A planning period is comprised of one or more increments.
RACK VOLUME EQUIVALENT A unit of volume that equals 36.0 cubic feet or 1.0193 cubic meters.
RECOVERABLE CARGO Cargo that is removed from the ISS and returned to Earth to be refurbished for future use, samples for evaluation, or items to be examined as part of sustaining engineering.
RESOURCES Identifies a particular subset of ISS on-orbit capabilities used in support of system and utilization operations. It includes the following: A. Average power kW
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B. Crew time (hours) C. Communications D. On-orbit accommodations (pressurized and unpressurized) E. Transportation Mass F. Transportation Volume
S-BAND 1550 to 5200 Megahertz
SCHEDULED EXTRAVEHICULAR ACTIVITY An EVA planned prior to the start of an increment or flight/stage with nominal crew training and included in the nominal mission timeline.
SHORT DURATION BIOASTRONAUTICS INVESTIGATION A medical research payload that will be flown and returned in a pressurized volume on the same Shuttle flight, involves a Shuttle (non-ISS) crewmember(s) as the test subject, and does not require any ISS resources (e.g., ISS crew time, ISS power, ISS communications) to accomplish the research objective. Responsibility for manifesting and prioritizing Short Duration Bioastronautics Investigations (SDBIs) with respect to the other ISS payloads resides with the ISS Payloads Office. However, responsibility for planning SDBI activities and resources during the mission, as well as Certification of Flight Readiness (CoFR) for the SDBIs, resides with the Space Shuttle Program and will be accomplished in accordance with Space Shuttle Program processes and procedures.
SOFT COMMIT Amount of resources estimated to be available to utilization based on either estimated capabilities above specified conditions/assumptions, a reduction of system reserves, or both.
STAGE Period of on-orbit configuration of the ISS after each flight which adds capability to the ISS. This can also refer to a designated period between launch vehicles defined by the ISS Program for requirement documentation and planning purposes.
SYSTEMS A group of H/W that collectively supports or provides capabilities to the orbiting ISS. In general, anything other than utilization. Specifically included in this set are assembly, logistics/maintenance environmental support, power, etc.
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TASK TYPE DESIGNATOR Identifies categories for mission task requirements and include: [Extravehicular Activity (EVA)], [Intravehicular Activity (IVA)], [Robotics], [Robotic On-Board Trainer (ROBoT)], [Utilization], [Ground], [Jettison] and [Imagery].
TRANSFER To remove H/W and/or provisions from one vehicle or module and place onto another vehicle or module.
TRANSFER VEHICLE A transportation vehicle that provides capability to move mass and volume from the insertion orbit to ISS and from ISS to reentry.
TRANSPORTATION VEHICLE A vehicle that docks to the ISS to deliver provisions, cargo, and/or crew for ISS operations.
UNSCHEDULED EXTRAVEHICULAR ACTIVITY An EVA resulting from unforeseen developments during a mission and not included in the nominally scheduled mission activities, but which may be required to achieve ISS Program mission success.
USOS (UNITED STATES ON-ORBIT SEGMENT) Term that generically describes ISS hardware and software systems manufactured and installed on-orbit by NASA. Within this document, examples of USOS include the truss solar arrays for the generation of power and the Joint Airlock, EMU suit, tools and associated hardware for NASA based EVAs.
UTILIZATION The set of requirements associated with research experiment integration and operation.
VALIDATION The process of formally approving the developed process, services, or products at the conclusion of operational test and evaluation. This approval indicates developed processes, services, or products satisfy their intended operational mission.
VERIFICATION The activities which assure that each level of requirements (including test requirements) or specifications correctly echoes the intentions of the immediately superior level of requirements.
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APPENDIX C
OPEN WORK
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APPENDIX C - OPEN WORK
Table C-1 lists the specific To Be Determined (TBD) items in the document that are not yet known. The TBD is inserted as a placeholder wherever the required data is needed and is formatted in bold type within brackets. The TBD item is numbered based on the section where the first occurrence of the item is located as the first digit and a consecutive number as the second digit (i.e.,
TABLE C-1 TO BE DETERMINED ITEMS
TBD Section Description Status 1-1 1.2, Figure 3.1-1, Data in work. To be baselined in IDRD Flight Program. Open Table 3.2-1, Table 3.3-1 1-2 1.2, 2.1, Table SSP 54016 has not been published. Open 3.3-1 1-3 1.2, 2.1 SSP 54015-14S has not been published. Open 1-4 1.2, 2.1 SSP 54015-26P has not been published. Open 1-5 1.2, 2.1 SSP 54015-ATV1 has not been published. Open 1-6 1.2, 2.1 SSP 54015-13A.1 has not been published. Open 1-7 1.2, 2.1 SSP 54015-27P has not been published. Open 1-8 1.2, 2.1 SSP 54015-10A has not been published. Open 1-9 1.2, 2.1 SSP 54015-ANX 2 has not been published. Open 1-10 1.2, 2.1 SSP 54015-ANX 3 has not been published. Open 1-11 1.2, 2.1 SSP 54015-ANX 4 has not been published. Open 1-12 1.2, 2.1 SSP 54015-ANX 5 has not been published. Open 1-13 1.3, 2.1 SSP 543XX, Post Increment Evaluation Report for Increment 15 has not Open been published. 2-1 2.2 SSP 54014-13S has not been published. Open 2-2 2.2 SSP 54014-25P has not been published. Open 2-3 2.2 SSP 543XX, Post Increment Evaluation Report for Increment 14 has not Open been published. 3-1 Table 3.2-1, Date of the 14 Soyuz relocation from the SM Aft port to the FGB Nadir Open Table 3.3-1 port is not yet defined. 3-2 Table 3.3-1 Increment 15 crew assignment is to be determined. Open 3-3 Table 3.3-1 ISS 12A.1 FE crew assignment is to be determined. Open 3-4 Table 3.3-1 ISS 10A FE crew assignment is to be determined. Open 3-5 Table 3.3-1 Data for Table 3.3-1 will be supplied upon the baselining of the IDRD. Open 3-6 Table 3.3-1 ISS 10A FE returns in the strategic time frame. Open 4-1 Table 4.4-1 Communication coverage percent columns data source to be determined. Open 4-2 Table 4.5-1 Additional Resource Requirements for Increment 15 are to be Open determined.
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TABLE C-1 TO BE DETERMINED ITEMS
TBD Section Description Status 5-1 Table 5.0-1 ATV1 atmospheric gas quantities per tank set are to be determined. Open Decision will be made at L-4 months between O2 and Air amounts. 5-2 Table 5.0-1 ESA is assessing a case allocating 1977kg for prop support, 6 racks plus Closed adapter plates, and 1765kg total of dry cargo. 5-3 Table 5.0-1a Power allocation for utilization has not been determined. Open 5-4 Table 5.0-1 Mass and volume data to be provided at a later date. Open 6-1 6.2.1,Table 3.3-1 Russian Science Experiment List is to be determined. Open 6-2 6.2.2.1 ATV1 mission propellant requirements have not been defined. Open 6-3 6.4.2, 6.4.3.8, ATV Docking/Undocking Constraints have yet to be fully determined. Open 6.4.6.1, 6.8.2, 6.8.3.5 6-4 6.3.2 Visiting crew operations during Flight 14S to be determined. Open 6-5 6.5.2, 6.5.3.1, Altitudes to be determined. Open 6.7.2, 6.7.3.1
6-6 6.7.2 O2/N2 transfer number to be determined. Open 6-7 6.4.3.8, An angle different from 65 degrees, provides less or no power generation Open by the SM. A specific positioning angle that satisfies best power generation is beta angle dependent and has not been analyzed at this time. 6-8 6.7.2 Need to determine if OBSS sensor package will be certified for on-board Open ISS stowage and operations. A-1 Appendix A Acronym definition to be provided. Closed D-1 Appendix D Table D.2-1 data will be provided at a later date. Closed H-1 6.4.2, 6.6.2, On-orbit Checkout Requirements will be provided at a later date. Open Appendix H I-1 6.5.2, Appendix I 13A.1 Transfer Priority List is undefined. Open I-2 6.4.2, Appendix I ATV1 Transfer Priority List is undefined. Open I-3 6.7.2, Appendix I 10A Transfer Priority List is undefined. Open J-1 6.3.2, 6.4.2, ONS to be provided at a later date. Closed 6.5.2, 6.6.2, 6.7.2, 6.8.2, Appendix J K-1 6.3.2, To be provided at a later date. Open Appendix K
Table C-2 lists the specific To Be Resolved (TBR) issues in the document that are not yet known. The TBR is inserted as a placeholder wherever the required data is needed and is formatted in bold type within brackets. The TBR issue is numbered based on the section where the first occurrence of the issue is located as the first digit and a consecutive number as the second digit (i.e.,
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TABLE C-2 TO BE RESOLVED ITEMS
TBR Section Description Status FP 3-2 Figure 3.1-1, Table Launch date is under review with the Shuttle Program. Closed 3.2-1 FP 3-6 Figure 3.1-1, This date has been identified as No Earlier Than (NET) by the Open Table 3.2-1, Shuttle Program. Table 3.3-1 FP 3-7 Figure 3.1-1, Dates are under review to resolve GGR&C conflicts. Open Table 3.2-1, Table 3.3-1 FP 3-8 Figure 3.1-1, Russian Flight Program is under review. The Russian Flight Program Open Table 3.2-1, may change due to absent Partner commitments for crew rotation, Table 3.3-1 crew rescue, and ISS habitation. FP 3-31 2.1, 2.2, ATV1 launch date has been identified as No Earlier Than (NET) by Open Figure 3.1-1, ESA. ATV1 dates are under review. Table 3.2-1 PAL undock date violates GGR&C # H.2.13.B. FP 3-32 Figure 3.1-1, Table Proper lighting conditions required for visual monitoring of the final Open 3.2-1 approach in the +XVV +Z Nadir attitude over Russian Ground Sites are not available on the proposed docking date. FP 3-33 Figure 3.1-1, Dates are under review to address planning for Stage 15S. Initial Open Table 3.2-1 stage duration assessment results indicate a required minimum of 43 days, which is not provided by current planning. Strategic assessment and incorporation of maximum delay of 1E launch date to No Earlier Than 10/17/07 does not result in sufficient minimum stage duration; therefore, 15S launch date acceleration to 8/27/07 must also be addressed. 4-1 Table 4.2-1, 6.3.2, Crew time calculation still in work. Open 6.4.2, 6.6.2, 6.8.2 6-1 6.3.2, 6.4.2 Details of Orbiter TPS Inspection will be provided upon Closed recommendation from Shuttle Return to Flight Team. 6-2 6.5.2 Assessment of changes to the Flight Program definition as a result Open of the ESP-3 addition to Flight 13A.1 is not complete. 6-3 6.7.3.9 Loads analysis is being reviewed to determine if Beta Gimbal locking Open is required for this operation. 6-4 6.4.4.2 Tasks are not currently certified due to hardware constraints. Open 6-5 6.3.2, 6.4.2, 6.6.2, GGR&C CR to reduce med ops allocation from 12 to 10 hours has Closed 6.8.2 not been approved. 6-6 6.4.4.2, 6.6.4.2, The readiness of these tasks is based upon generic development of Open 6.8.4.2 the procedures to a level that can be validated against a set of criteria. Definition and program agreement on the criteria determining generic task readiness needs to be resolved. Final development of these procedures will be required based upon actual configurations, locations and environmental conditions. 6-7 6.4.4.2 On-Orbit hardware deficiencies may preclude successful Heat Open Exchanger R&R. 6-8 6.7.4.2, 6.7.5.2 Pending analysis and approval by Program that these items can be Open safely jettisoned. 6-9 6.4.2 Pending decision on Russian power transfer architecture that affects Open fault tolerance of power transfer to the FGB. 6-10 6.6.2 Schedule in this stage if not performed before Flight 13A.1. Open 6-11 6.5.2 The priority of late Orbiter inspection is under review, pending Open analysis of MMOD risk for increased mission duration (with SSPTS)
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APPENDIX D
TOPOLOGIES
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APPENDIX D - TOPOLOGIES
D.1 GENERAL
This appendix provides an overview of the internal on-orbit topologies for Node 1, the U.S. Lab, and the Joint Airlock. Figures are included for each planned change of rack locations. Subrack topologies are included for the EXpedite the PRocessing of Experiments to the Space Station (EXPRESS) Racks located in the U.S. Lab.
D.2 ON-ORBIT RACK DESCRIPTIONS
Table D.2-1, On-Orbit Rack Descriptions, shows the description of the rack represented by each rack subelement number in the topologies contained in this appendix.
TABLE D.2-1 ON-ORBIT RACK DESCRIPTIONS
Rack SE# Rack Description 2 US Lab CCAA/Low Temperature TCS 3 US Lab CCAA/Moderate Temperature TCS
4 US Lab Avionics 1/Condensate H2O 5 US Lab Avionics 2 6 US Lab Avionics 3 7 US Lab DDCU #1 8 US Lab ARS 9 US Lab DDCU #2 11 US Lab MSS Avionics and Console/Storage 12 Cupola MSS Avionics and Console/Storage 13 NASA ISPR: HRF Rack #1 14 NASA ISPR: EXPRESS Rack #1 15 NASA ISPR: EXPRESS Rack #2 16 NASA ISPR: EXPRESS Rack #3 17 NASA ISPR: EXPRESS Rack #4 18 NASA ISPR: MSG 23 NASA ISPR: EXPRESS Rack #5 25 MELFI 27 TESS 28 US Lab Temporary CHeCS 110 ZSR 111 ZSR 116 ZSR 117 ZSR 118 ZSR 120 ZSR 155 RSR
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Rack SE# Rack Description 156 RSR 191 Airlock Stowage Platform - Overhead 192 Airlock Stowage Platform - Deck 193 Airlock Cabin Air Equipment Rack 194 Airlock Avionics Rack 301 DDCU 302 DDCU 303 DDCU 304 DDCU 313 OGS 381 U.S. Stowage Rack 417 NASA ISPR: HRF Rack #2
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D.3 NODE 1 TOPOLOGY
Figure D.3-1, Flights 14S, 13A.1 and 10A Node 1 Topology, shows a high level overview of the Node 1 on-orbit topology at the beginning of the increment. Refer to Table D.2-1 for a definition of the rack SE numbers.
NOD1O4
Z1 Truss ZSR OVERHEAD SE#110
NOD1S4
STARBOARD Airlock ZSR SE#116
FORWARD NOD1D4 AFT
DECK Node 3* RSR SE#381
NOD1P4
PORT ZSR SE#111
* Shading indicates a future or unused interface FIGURE D.3-1 FLIGHT 14S, 13A.1 AND 10A NODE 1 TOPOLOGY
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D.4 NODE 2 TOPOLOGY
Figure D.4-1, Flight 10A Node 2 Topology, shows a high level overview of the Node 2 on-orbit topology at the beginning of the increment. Refer to Table D.2-1 for a definition of the rack SE numbers.
NOD1O4 NOD1O5
DDCU ZSR OVERHEAD SE#301 SE#118
NOD1S4 NOD1S5
Columbus STARBOARD DDCU RSR SE#302 SE#155
FORWARD NOD1D4 NOD1D5 AFT
DECK MPLM* DDCU ZSR SE#303 SE#120
NOD1P4 NOD1P5
PORT JEM DDCU RSR SE#304 SE#156
* Shading indicates a future or unused interface FIGURE D.4-1 FLIGHT 10A NODE 2 TOPOLOGY
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D.5 FLIGHTS 14S, 13A.1 AND 10A UNITED STATES LABORATORY TOPOLOGY
Figure D.5-1, Flights 14S, 13A.1 and 10A United States Laboratory Topology, shows a high level overview of the U.S. Lab on-orbit topology after Flight ULF1.1. Refer to Table D.2-1 for a definition of the rack SE numbers.
LAB1O1 LAB1O2 LAB1O3 LAB1O4 LAB1O5 LAB1O6
EXPRESS#2 EXPRESS#3 ZSR EXPRESS#1 MELFI DDCU#2 (ARIS) (ARIS) SE#117 OVERHEAD SE#14 SE#9 SE#15 SE#16 SE#25
Cupola MSS/ CCAA/ TESS HRF#1 MSG EXPRESS#5 Avionics & Moderate STARBOARD SE#27 SE#13 SE#18 SE#23 Console TCS SE#3 SE#12 LAB1S1 LAB1S2 LAB1S3 LAB1S4 LAB1S5 LAB1S6 FORWARD AFT
Avionics Avionics Window Temp Avionics #1/ ARS Cond H2O DECK #2 #3 CHeCS SE#8 SE#5 SE#6 SE#28 SE#4 LAB1D1 LAB1D2 LAB1D3 LAB1D4 LAB1D5 LAB1D6 LAB1P1 LAB1P2 LAB1P3 LAB1P4 LAB1P5 LAB1P6 Lab MSS/ PORT EXPRESS#4 HRF#2 OGS DDCU#1 Avionics & CCAA/ SE#313 SE#17 SE#7 Console Low TCS SE#417 SE#2 SE#11
FIGURE D.5-1 FLIGHTS 14S, 13A.1 AND 10A UNITED STATES LABORATORY TOPOLOGY
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D.6 JOINT AIRLOCK TOPOLOGY
Figure D.6-1, Flights 14S, 13A.1 and 10A Joint Airlock Topology, shows a high level overview of the Airlock on-orbit topology. Refer to Table D.2-1 for definitions of rack SE numbers.
AIR1O1
A/L Stowage OVERHEAD SE#191
AIR1A1
AFT A/L Avionics SE #194
Node 1 AIR1D1
DECK A/L Stowage SE#192
AIR1F1
FORWARD Cabin Air Equipment SE #193
FIGURE D.6-1 FLIGHTS 14S, 13A.1 AND 10A JOINT AIRLOCK TOPOLOGY
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APPENDIX E
INCREMENT CONFIGURATIONS
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APPENDIX E - INCREMENT CONFIGURATIONS
The configuration plans for flight and stage are in JSC 26557, On-orbit Assembly, Modeling, and Mass Properties Data Book, also known as Blue Book, accessible through Electronic Document Management System (EDMS).
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APPENDIX F
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APPENDIX F -
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APPENDIX G
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APPENDIX G
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APPENDIX H
ON-ORBIT CHECKOUT REQUIREMENTS
[No Russian Review Required]
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APPENDIX H - ON-ORBIT CHECKOUT REQUIREMENTS
Appendix H contains a listing of those MSS OCRs that can be completed during this increment. All Tables have been scrubbed to eliminate completed OCRs or OCRs that cannot be accomplished within this increment. Table H-1 Part 1 of this plan contains SSRMS OCRs from the previous increment not completed and carried forward. Table H-2 contains MBS OCRs. Table H-3 contains MSS Periodic checkout tasks due for completion within this increment. With the exception of Periodic and Conditional OCRs, the tasks in this matrix, as well as those planned in other increments, must be completed for CSA to consider the SSRMS and MBS fully commissioned. Periodic/Data Trending checkout tasks are described where ‘start of life’ baseline data sets are required in this increment. Periodic checkouts will be further addressed in the IDRDs for subsequent Increments. Changes to requirements should be addressed to CSA via the Manager, Mission Operations. Changes to requirements during real-time operations should be addressed to the ISS Management Center.
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TABLE H-1 REMAINING SSRMS ON-ORBIT CHECKOUT REQUIREMENT TASKS FROM PREVIOUS INCREMENTS (PAGE 1 OF 2)
Checkout Description Type of OCR Required Priority and Required Comments Task (Note 3) Operations-Phase (Joint (Note 4) Operations/Stage Operations, Options) (Notes 5-8)
One- Period Condition Desirab Highly Mandatory Crew Time Time ic al le Desirabl (Note 6) and Special
From SSP 54102 Activati e MCC/ISS/
Part 1: OCR Number on Shuttle Resources (Notes 10-13) 6 FMS FMS data is X Assembl 10 minutes Some data was characterizatio collected at valuable y additional collected during n during dynamic motion operation crew time at PP2 and PP4 nominal opportunities (i.e., s with each data collection is dynamic pre-identified which large/hea opportunity highest priority operations (i.e., provide rich FMS vy (concurrent on LEE A tip a constrained data). payloads with redundant string APPC, heavy Required to close handled nominal/other and LEE B tip payload out NASA/CSA by Ops like Prime string for stops/starts). SSRMS; DTO 264 which no loaded agreements for - For BITE Waivers and CoFR until during Flight data has been complete 9A payload collected. check, truth Exceptions related model to the FMS/FMA maneuvers) Additional validation opportunities will be identified and - Data from both strings agreed to serve for FMS raw or and both LEEs reported data collection using required (see comments for Normal Format Telemetry, with priorities) EDD or NDD - Remaining desirable. This LEE/ String will also provide combination data for MDSF - LEE A - model validation, Redundant FMS BITE tolerance - LEE B - adequacy. Prime
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TABLE H-1 REMAINING SSRMS ON-ORBIT CHECKOUT REQUIREMENT TASKS FROM PREVIOUS INCREMENTS (PAGE 2 OF 2)
Checkout Description Type of OCR Required Priority and Required Operations- Comments Task (Note 3) Phase (Joint Operations/Stage (Note 4) Operations, Options) (Notes 5-8)
One- Periodi Condition Desirabl Highly Mandatory Crew Time and Time c al e Desirable (Note 6) Special Activati MCC/ISS/
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Part 1: OCR Number Resources (Notes 10-13) 45 SSRMS Thermal Thermal trending data X X FMS thermal drift Data Analysis has been collected on data is needed to FMS Thermal both strings and LEEs. optimize and Analysis of the data adjust the thermal Drift Analysis has indicated compensation For FMS additional data algorithm in the objectives, test is collections will be SSRMS software, eventually required: as well as to required with FMS Saturation troubleshoot the each LEE as tip LEE A Prime Troubleshooting (as well as both sensor saturation strings). These will be detailed issue. using the Chit Secondary Data collection for process, referencing objectives; this parent brief periods of LOS during the SSRMS Thermal requirement. Trending selected orbit will FMS saturation be acceptable. Baseline data for troubleshooting was Required to close thermal models performed on June out NASA/CSA 9/10, 2003. One more LEE rigidize load agreements for test remains to see if cell drift analysis waivers and CoFR the FMS retains its exceptions related calibration status to the FMS/FMA. when temperature falls below 5 degrees Celsius, and to check performance with the new Thermal Protection Kit.
57 Joint Direct Drive SSRMS Joints are X Within 1 year 60 minutes Test driven using modified of uplink of crew time JCS to provide direct required (estimated); this drive to motors. This configuration could be will provide individual file changes reduced/ joint performance eliminated with baseline for trending MSS Ground and degradation Control assessment.
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TABLE H-2 MRS BASE SYSTEM ON-ORBIT CHECKOUT REQUIREMENTS
Task Checkout Description Type of OCR Required Priority and Required Operations- Comments Number Task Phase (Joint Operations/Stage Operations, Options)
One-Time Periodic Conditional Desirable Highly Mandatory Special Activation Desirable MCC/ISS/ Shuttle Resources
TABLE H-3 PERIODIC ON-ORBIT CHECKOUT REQUIREMENT TASKS
Checkout Description Type of OCR Required Priority and Required Operations-Phase Comments Task (Note 3) (Joint Operations/Stage Operations, (Note 4) Options) (Notes 5-8) One-Time Periodic Conditional Desirable Highly Mandatory Crew Time Activation Desirable (Note 6) and Special MCC/ISS/ Task Number Shuttle Resources (Notes 10-13) MSS Detection of Determination of X Annually MCC-H Setup details are Camera CLA and CLPA source of only in accordance OCR 001 camera defects is with CSA deterioration accomplished Camera OCR from Dead by viewing white Plans: SSRMS Pixels/ and black OCRs 001/003 Contamination/ surfaces since and MBS OCR Micrometeoroi this is where 001. d Debris defects are damage. most apparent. Determination of source of defects is performed offline. MSS Determination Cycle power to X Annually MCC-H Set-up details Camera of whether a camera lights only are in OCR 002 single bulb has while observing accordance with failed on the via separate CSA Camera light assembly camera view. OCR Plans: SSRMS OCRs 002/004 and MBS OCR 002.
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APPENDIX I
SHUTTLE FLIGHT AND ATV TRANSFER PRIORITY LISTS
[Items for Russian Review will be Identified with (RUSSIAN)]
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APPENDIX I - SHUTTLE FLIGHT AND ATV TRANSFER PRIORITY LISTS
I.1 Flight 13A.1 Integrated Middeck Launch and Return Priorities
The following items comprise the Flight 13A.1 Transfer Priority List. Items that are transferred from ISS to Shuttle are differentiated by the (r) designation from those transferred from Shuttle to ISS. The transfer items are grouped according to the transfer priorities and reference associated mission priorities as specified in Section 6.
I.2 ATV1 Integrated Middeck Launch and Return Priorities
The following items comprise the ATV1 Transfer Priority List. Items that are transferred from ISS to ATV1 are differentiated by the (r) designation from those transferred from ATV1 to ISS. Some items will be stowed in ATV1 and not transferred.
I.3 Flight 10A Integrated Middeck Launch and Return Priorities
The following items comprise the Flight 10A Transfer Priority List. Items that are transferred from ISS to Shuttle are differentiated by the (r) designation from those transferred from Shuttle to ISS. The transfer items are grouped according to the transfer priorities and reference associated mission priorities as specified in Section 6.
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APPENDIX J
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APPENDIX J -
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APPENDIX K
USOS Resources To Be Provided For Flight 14S Visiting Crewmember
(REQUIREMENTS BETWEEN NASA AND INTERNATIONAL PARTNER)
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APPENDIX K
Table K-1, USOS Resources to be Provided for X International Partner/X Crewmember, is limited to the below-listed and agreed-to resources that NASA will provide to the X crewmember during this mission on X Soyuz. The listing of utilization to be performed during the X Soyuz mission will be provided via Rocket Space Corporation - Energia (RSC-E) and is listed in the main document under Section 6.2, Increment 15 Specific Requirements. NASA agrees to provide the following resources and will be compensated by X.
TABLE K-1 USOS RESOURCES TO BE PROVIDED FOR X INTERNATIONAL PARTNER/X CREWMEMBER
Resource Agreements E-mail IP Phone Timeline Procedures Lab Facilities Ham * Not solely a USOS resource - International Hardware Imagery PAO Medical Crew Provisions: Exercise Equipment Video Down Up/Downlink Data (includes OCA) Ground Support Preflight Crew Training for Prime and Backup X Crewmembers
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