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Contingency Shuttle Crew Support (Cscs)/Rescue Flight Resource Book
CSCS/Rescue Flight Resource Book JSC-62900 CONTINGENCY SHUTTLE CREW SUPPORT (CSCS)/RESCUE FLIGHT RESOURCE BOOK OVERVIEW 1 Mission Operations CSCS 2 Directorate RESCUE 3 FLIGHT DA8/Flight Director Office Final July 12, 2005 National Aeronautics and Space Administration Lyndon B. Johnson Space Center Houston, Texas FINAL 07/12/05 2-i Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 CONTINGENCY SHUTTLE CREW SUPPORT (CSCS)/RESCUE FLIGHT RESOURCE BOOK FINAL JULY 12, 2005 PREFACE This document, dated May 24, 2005, is the Basic version of the Contingency Shuttle Crew Support (CSCS)/Rescue Flight Resource Book. It is requested that any organization having comments, questions, or suggestions concerning this document should contact DA8/Book Manager, Flight Director Office, Building 4 North, Room 3039. This is a limited distribution and controlled document and is not to be reproduced without the written approval of the Chief, Flight Director Office, mail code DA8, Lyndon B. Johnson Space Center, Houston, TX 77058. FINAL 07/12/05 2-ii Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 1.0 - OVERVIEW Section 1.0 is the overview of the entire Contingency Shuttle Crew Support (CSCS)/Rescue Flight Resource Book. FINAL 07/12/05 2-iii Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 This page intentionally blank. FINAL 07/12/05 2-iv Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 2.0 - CONTINGENCY SHUTTLE CREW SUPPORT (CSCS) 2.1 Procedures Overview.......................................................................................................2-1 2.1.1 ................................................................................ -
L AUNCH SYSTEMS Databk7 Collected.Book Page 18 Monday, September 14, 2009 2:53 PM Databk7 Collected.Book Page 19 Monday, September 14, 2009 2:53 PM
databk7_collected.book Page 17 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS databk7_collected.book Page 18 Monday, September 14, 2009 2:53 PM databk7_collected.book Page 19 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS Introduction Launch systems provide access to space, necessary for the majority of NASA’s activities. During the decade from 1989–1998, NASA used two types of launch systems, one consisting of several families of expendable launch vehicles (ELV) and the second consisting of the world’s only partially reusable launch system—the Space Shuttle. A significant challenge NASA faced during the decade was the development of technologies needed to design and implement a new reusable launch system that would prove less expensive than the Shuttle. Although some attempts seemed promising, none succeeded. This chapter addresses most subjects relating to access to space and space transportation. It discusses and describes ELVs, the Space Shuttle in its launch vehicle function, and NASA’s attempts to develop new launch systems. Tables relating to each launch vehicle’s characteristics are included. The other functions of the Space Shuttle—as a scientific laboratory, staging area for repair missions, and a prime element of the Space Station program—are discussed in the next chapter, Human Spaceflight. This chapter also provides a brief review of launch systems in the past decade, an overview of policy relating to launch systems, a summary of the management of NASA’s launch systems programs, and tables of funding data. The Last Decade Reviewed (1979–1988) From 1979 through 1988, NASA used families of ELVs that had seen service during the previous decade. -
Commercial Orbital Transportation Services
National Aeronautics and Space Administration Commercial Orbital Transportation Services A New Era in Spaceflight NASA/SP-2014-617 Commercial Orbital Transportation Services A New Era in Spaceflight On the cover: Background photo: The terminator—the line separating the sunlit side of Earth from the side in darkness—marks the changeover between day and night on the ground. By establishing government-industry partnerships, the Commercial Orbital Transportation Services (COTS) program marked a change from the traditional way NASA had worked. Inset photos, right: The COTS program supported two U.S. companies in their efforts to design and build transportation systems to carry cargo to low-Earth orbit. (Top photo—Credit: SpaceX) SpaceX launched its Falcon 9 rocket on May 22, 2012, from Cape Canaveral, Florida. (Second photo) Three days later, the company successfully completed the mission that sent its Dragon spacecraft to the Station. (Third photo—Credit: NASA/Bill Ingalls) Orbital Sciences Corp. sent its Antares rocket on its test flight on April 21, 2013, from a new launchpad on Virginia’s eastern shore. Later that year, the second Antares lifted off with Orbital’s cargo capsule, (Fourth photo) the Cygnus, that berthed with the ISS on September 29, 2013. Both companies successfully proved the capability to deliver cargo to the International Space Station by U.S. commercial companies and began a new era of spaceflight. ISS photo, center left: Benefiting from the success of the partnerships is the International Space Station, pictured as seen by the last Space Shuttle crew that visited the orbiting laboratory (July 19, 2011). More photos of the ISS are featured on the first pages of each chapter. -
Upper Stages Using Liquid Propulsion and Metallized - Propellants
NASA NASA-TP-3191 19920007933 Technical Paper 3191 February 1992 Upper Stages Using Liquid Propulsion and Metallized - Propellants NASA NASA Technical Paper 3191 1992 Upper Stages Using Liquid Propulsion and Metallized Propellants Bryan A. Palaszewski Lewis Research Center Cleveland, Ohio NASA National Aeronauticsand Space Administration Office of Management Scientific and Technical InformationProgram Summary (Isp)may be required. Also, because of the limits of the capa- bilityof the IUS and potentiallylimitedavailabilityof the Titan Metallized propellants are liquid propellants with a metal IV/Centaur G-Prime for NASA missions, alternativesto these additive suspended in a gelled fuel. Typically, aluminum par- stages should be considered. ticles are the metal additive. These propellants increase the The largest available stage for the STS is the Inertial Upper density and/or the specific impulse of the propulsion system. Stage (IUS, ref. 1). It can deliver a 2268-kg (5000-Ibm)pay- Usingmetallized propellantsfor volume-and mass-constrained loadto geosynchronousEarth orbit (GEO).However, for plane- upper stages can deliver modest increases inperformance for tary missions, the IUS is limited to low-energy missions. The low Earth orbit to geosynchronous Earth orbit (LEO-GEO) t Galileo mission to Jupiter (ref. 2) was launched on an IUS. and other Earth-orbital transfer missions. However, using Using the Space Transportation System (STS)/IUS, its flight metallized propellants for planetary missionscan deliver great time will be 6.5 yr. With a high-performance cryogenic upper reductions in flight time with a single-stage, upper-stage stage, the flight time could havebeen reduced to 1.5 yr. There system, is not, however, any cryogenic upper stage available that is Tradeoff studies comparing metallized propellant stage compatible with the STS (refs. -
+ Part 17: Acronyms and Abbreviations (265 Kb PDF)
17. Acronyms and Abbreviations °C . Degrees.Celsius °F. Degrees.Fahrenheit °R . Degrees.Rankine 24/7. 24.Hours/day,.7.days/week 2–D. Two-Dimensional 3C. Command,.Control,.and.Checkout 3–D. Three-Dimensional 3–DOF . Three-Degrees.of.Freedom 6-DOF. Six-Degrees.of.Freedom A&E. Architectural.and.Engineering ACEIT. Automated.Cost-Estimating.Integrated.Tools ACES . Acceptance.and.Checkout.Evaluation.System ACP. Analytical.Consistency.Plan ACRN. Assured.Crew.Return.Vehicle ACRV. Assured.Crew.Return.Vehicle AD. Analog.to.Digital ADBS. Advanced.Docking.Berthing.System ADRA. Atlantic.Downrange.Recovery.Area AEDC. Arnold.Engineering.Development.Center AEG . Apollo.Entry.Guidance AETB. Alumina.Enhanced.Thermal.Barrier AFB .. .. .. .. .. .. .. Air.Force.Base AFE. Aero-assist.Flight.Experiment AFPG. Apollo.Final.Phase.Guidance AFRSI. Advanced.Flexible.Reusable.Surface.Insulation AFV . Anti-Flood.Valve AIAA . American.Institute.of.Aeronautics.and.Astronautics AL. Aluminum ALARA . As.Low.As.Reasonably.Achievable 17. Acronyms and Abbreviations 731 AL-Li . Aluminum-Lithium ALS. Advanced.Launch.System ALTV. Approach.and.Landing.Test.Vehicle AMS. Alpha.Magnetic.Spectrometer AMSAA. Army.Material.System.Analysis.Activity AOA . Analysis.of.Alternatives AOD. Aircraft.Operations.Division APAS . Androgynous.Peripheral.Attachment.System APS. Auxiliary.Propulsion.System APU . Auxiliary.Power.Unit APU . Auxiliary.Propulsion.Unit AR&D. Automated.Rendezvous.and.Docking. ARC . Ames.Research.Center ARF . Assembly/Remanufacturing.Facility ASE. Airborne.Support.Equipment ASI . Augmented.Space.Igniter ASTWG . Advanced.Spaceport.Technology.Working.Group ASTP. Advanced.Space.Transportation.Program AT. Alternate.Turbopump ATCO. Ambient.Temperature.Catalytic.Oxidation ATCS . Active.Thermal.Control.System ATO . Abort-To-Orbit ATP. Authority.to.Proceed ATS. Access.to.Space ATV . Automated.Transfer.Vehicles ATV . -
The National Aeronautics and Space Administration: Overview, FY2004 Budget in Brief, and Issues for Congress
Order Code RS21430 Updated April 15, 2003 CRS Report for Congress Received through the CRS Web The National Aeronautics and Space Administration: Overview, FY2004 Budget in Brief, and Issues for Congress Marcia S. Smith Specialist in Aerospace and Telecommunications Policy Resources, Science, and Industry Division Summary The National Aeronautics and Space Administration (NASA) was created in 1958 to conduct U.S. government civilian space activities (military space activities are under the purview of the Department of Defense). The FY2004 budget request for NASA is $15.5 billion, compared with its FY2003 appropriations level of $15.3 billion. During consideration of that request, attention is expected to focus on the investigation of the February 1, 2003 space shuttle Columbia tragedy (see CRS Report RS21408) and its implications for NASA and the space program as a whole. A more detailed analysis of NASA’s FY2004 request is available in CRS Report RL31821. This report will be updated as events warrant. Agency Overview The National Aeronautics and Space Administration (NASA) was created by the 1958 National Aeronautics and Space Act (P.L. 85-568). NASA’s charter is to conduct civilian space and aeronautics activities. Military space and aeronautics activities are conducted by the Department of Defense (DOD) and the intelligence community. DOD and NASA cooperate in some areas of technology development and occasionally have joint programs. NASA opened its doors on October 1, 1958, almost exactly one year after the Soviet Union ushered in the Space Age with the launch of the world’s first satellite, Sputnik, on October 4, 1957. In the more than 40 years that have elapsed, NASA has conducted far reaching programs in human and robotic spaceflight, technology development, and scientific research. -
SPACE TRANSPORTATION Contents
Chapter 5 SPACE TRANSPORTATION Contents Page Introduction. ..............103 The Space Transportation Industry . ................103 The providers of Space Transportation Services . .. ...103 Buyers of Space Transportation Services . ................122 Competition in Space Transportation . ......125 Development of Competition . ............125 Assessment of Demand . .................126 Nature of Competition . .. ...128 Effects of Competition . .. ....134 Cooperation in Space Transportation . ..............137 Current Policies. ........................138 Future Policy Options.. .. ....140 List of Tables Table No. Page 5-1. Ariane Flights . ..........115 5-2. Transportation Costs to Geosynchronous Orbit . ......................132 5-3. NASA vs. Arianespace Financing . ..............133 5-4. Companies That Contribute to Manufacturing Japanese Launch Vehicles ..139 List of Figures Figure No. Page 5-1. U.S. Launch vehicles . ..............104 5-2.The Hermes Spaceplane . ..................116 5-3. Foreign National Comparative Launch Vehicle Development. ..........118 5-4. Projection of Future Space Shuttle Demand Rockwell International. ...127 5-5. Outside Users Payload Model Battelle’s Columbus Laboratories . .......,128 5-6. Low Model Market Share by Launch Vehicle . ...............129 5-7. High Model Market Share by Launch Vehicle . .......................130 5-8. Arianespace Financing . ..133 5-9. Rockwell International Estimates That the Shuttle is Most Economical Over ELVs at High-Volume Operations. ............................135 -
A Status Report Lockheed Launch Vehicle
I A STATUS REPORT LOCKHEED LAUNCH VEHICLE I for the 7th ANNUAL AIM-UTAH STATE UNIVERSITY I CONFERENCE ON SMALL SATEWTES D.E. Davis, J.W. AngelP, A.J. MaeLaren2 I Lockheed Missiles & Spaee Co.,lne Abstract: This paper discusses a new collocated product development team family of small and medium space launch with the mandate to use our engineering, vehicles being developed by Lockheed manufacturing, and flight test I Missiles & Space Company, Inc. The experience, but - and an important but development program will culminate in - to be innovative in our approaches. a demonstration launch in November For example we elected to use, as much I 1994. The paper gives a brief as possible, existing hardware; to use background and gives the program status aluminum structure rather than as of the date of this paper. composites - although Lockheed builds Supporting graphics are included. much composite structure; and to I simplify the way we do business. Background: We have streamlined our Lockheed Missiles & Space Co, paperwork system. The product I Inc. has been studying small space development team has informal reviews launch vehicles since 1987. The - informal in the sense that their are no original approach then was to use dry-runs, and hand drawn graphics are I surplus or excess ballistic missile acceptable. The technical caliber of assets, primarily the 1st and 2nd stages the presentations is as professional as if from the Poseidon C-3 missile as the it were our traditional government basis, replacing the weapon system customer instead of just ourselves. I guidance and control with state of the art Rather than tell our prospective technology, and adding a 3rd stage with subcontractors how they should design a Star 48 solid rocket motor. -
STS 30, 34 and 44- a Rebirth of the Planetary Missions
The Space Congress® Proceedings 1988 (25th) Heritage - Dedication - Vision Apr 1st, 8:00 AM STS 30, 34 And 44- A Rebirth Of The Planetary Missions Ed Bangsund Director of Space Systems Planning Boeing Aerospace Company Seattle, Washington Robert Knutson Planning Staff Administrator Boeing Aerospace Company Seattle, Washington Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Bangsund, Ed and Knutson, Robert, "STS 30, 34 And 44- A Rebirth Of The Planetary Missions" (1988). The Space Congress® Proceedings. 5. https://commons.erau.edu/space-congress-proceedings/proceedings-1988-25th/session-10/5 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. STS 30, 34 AND 44 - A REBIRTH OF THE PLANETARY MISSIONS Ed Bangsund Robert Knutson Director of Space Systems Planning Planning Staff Administrator Boeing Aerospace Company Boeing Aerospace Company Seattle, Washington Seattle, Washington before it takes up its final flight path to Jupiter. ABSTRACT This new type of trajectory has been dubbed VEEGA, for Venus-Earth-Earth Gravity Assist, No American planetary probe has been launched with arrival at Jupiter to occur six years later since the twin Voyager spacecraft in 1979- in November 1995. The scientific objectives However, within eighteen months beginning of the Galileo mission are investigation of (1) in April 1989, three interplanetary probes will chemical composition and physical state of be shot into deep space from Shuttle cargo Jupiter's atmosphere, (2) chemical composition bays using the Inertial Upper Stage (IUS) as and physical state of the Jovian satellites, and an upper stage booster. -
Draft Flight Results of the Chandra X-Ray Observatory
DRAFT FLIGHT RESULTS OF THE CHANDRA X-RAY OBSERVATORY INERTIAL UPPER STAGE SPACE MISSION R. Tillotson*, D. Knoben', R. Walter' The Boeing Company Seattle, Washington / ABSTRACT Under contract to NASA, a specially configured version of the Boeing developed Inertial Upper Stage (IUS) booster was provided by Boeing to deliver NASA's 1.5 billion dollar Chandra X-Ray Observatory satellite into a highly elliptical transfer orbit from a Shuttle provided circular park orbit. Subsequently, the final orbit of the Chandra satellite was to be achieved using the Chandra Intergral Propulsion System (IPS) through a series of IPS burns. On 23 July 1999 the Shuttle Columbia (STS-93) was launched with the IUS/Chandra stack in the Shuttle payload bay. Unfortunately, the Shuttle Orbiter was unexpectantly inserted into an off-nominal park orbit due to a Shuttle propulsion anomaly occurring during ascent. Following the IUS/Chandra on-orbit deployment from the Shuttle, at seven hours from liftoff, the flight proven IUS GN&C system successfully injected Chandra into the targeted transfer orbit, in spite of the off-nominal park orbit. This paper describes the IUS GN&C system, discusses the specific IUS GN&C mission data load development, analyses and testing for the Chandra mission, and concludes with a summary of flight results for the IUS part of the Chandra mission. * Principal Engineer; The Boeing Company, Seattle, Washington; Member AIAA # Principal Engineer; The Boeing Company, Seattle, Washington DRAFT Page 1 DRAFF INTRODUCTION The IUS vehicle was developed under contract to the Air Force Space and Missile Systems Center. The vehicle is designed to take payloads to geosynchronous or other orbits after being boosted to low earth orbit. -
Space Launch Vehicles: Government Activities, Commercial Competition, and Satellite Exports
Order Code IB93062 CRS Issue Brief for Congress Received through the CRS Web Space Launch Vehicles: Government Activities, Commercial Competition, and Satellite Exports Updated September 7, 2001 Marcia S. Smith Resources, Science, and Industry Division Congressional Research Service The Library of Congress CONTENTS SUMMARY MOST RECENT DEVELOPMENTS BACKGROUND AND ANALYSIS U.S. Launch Vehicle Policy From “Shuttle-Only” to “Mixed Fleet” Clinton Administration Policy U.S. Launch Vehicle Programs and Issues NASA’s Space Shuttle Program Future Launch Vehicle Development Programs DOD’s Evolved Expendable Launch Vehicle (EELV) Program Government-Led Reusable Launch Vehicle (RLV) Programs Private Sector RLV Development Efforts U.S. Commercial Launch Services Industry Congressional Interest Foreign Competition (Including Satellite Export Issues) Europe China Russia Ukraine India Japan LEGISLATION IB93062 09-07-01 Space Launch Vehicles: Government Activities, Commercial Competition, and Satellite Exports SUMMARY Launching satellites into orbit, once the X-33, suffered delays and on March 1, 2001 exclusive domain of the U.S. and Soviet gov- NASA decided to end the program. ernments, today is an industry in which compa- Companies developing new launch vehicles are nies in the United States, Europe, China, Rus- reassessing their plans, and NASA has initiated sia, Ukraine, Japan, and India compete. In the a new “Space Launch Initiative” (SLI) to United States, the National Aeronautics and broaden the choices from which it can choose Space Administration (NASA) continues to be a new RLV design. Some of the SLI funding responsible for launches of its space shuttle, and is going to companies that have been trying to the Air Force has responsibility for launches develop their own new launch vehicles. -
Table of Contents
THE CAPE Military Space Operations 1971-1992 by Mark C. Cleary 45th Space Wing History Office Table of Contents Preface Chapter I -USAF Space Organizations and Programs Table of Contents Section 1 - Air Force Systems Command and Subordinate Space Agencies at Cape Canaveral Section 2 - The Creation of Air Force Space Command and Transfer of Air Force Space Resources Section 3 - Defense Department Involvement in the Space Shuttle Section 4 - Air Force Space Launch Vehicles: SCOUT, THOR, ATLAS and TITAN Section 5 - Early Space Shuttle Flights Section 6 - Origins of the TITAN IV Program Section 7 - Development of the ATLAS II and DELTA II Launch Vehicles and the TITAN IV/CENTAUR Upper Stage Section 8 - Space Shuttle Support of Military Payloads Section 9 - U.S. and Soviet Military Space Competition in the 1970s and 1980s Chapter II - TITAN and Shuttle Military Space Operations Section 1 - 6555th Aerospace Test Group Responsibilities Section 2 - Launch Squadron Supervision of Military Space Operations in the 1990s Section 3 - TITAN IV Launch Contractors and Eastern Range Support Contractors Section 4 - Quality Assurance and Payload Processing Agencies Section 5 - TITAN IIIC Military Space Missions after 1970 Section 6 - TITAN 34D Military Space Operations and Facilities at the Cape Section 7 - TITAN IV Program Activation and Completion of the TITAN 34D Program Section 8 - TITAN IV Operations after First Launch Section 9 - Space Shuttle Military Missions Chapter III - Medium and Light Military Space Operations Section 1 - Medium Launch Vehicle and Payload Operations Section 2 - Evolution of the NAVSTAR Global Positioning System and Development of the DELTA II Section 3 - DELTA II Processing and Flight Features Section 4 - NAVSTAR II Global Positioning System Missions Section 5 - Strategic Defense Initiative Missions and the NATO IVA Mission Section 6 - ATLAS/CENTAUR Missions at the Cape Section 7 - Modification of Cape Facilities for ATLAS II/CENTAUR Operations Section 8 - ATLAS II/CENTAUR Missions Section 9 - STARBIRD and RED TIGRESS Operations Section 10 - U.S.