Getting in Your Space: Learning from Past Rendezvous and Proximity Operations
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Shuttle-Mir Rendezvous & [Locking Missions
/ tv -t_ ---Fi>{ NASA-TM-II2692 • _7, w- -_ ° ;: Fourth Report of the Task Force on the Shuttle-Mir Rendezvous & [locking Missions March 1, 1995 A Task Force of the NASA Advisory Council THOMAS P. STAFFORD 1006 Cameron Street Alexandria, VA 22314 March 1, 1995 Dr. Bradford Paxkinson Chairman, National Aeronautics and Space Administration Advisory Council National Aeronautics and Space Administration Washington, DC 20546-0001 Dear Dr. Parkinson: Enclosed is the fourth report of the NAC Task Force on the Shuttle-Mir Rendezvous and Docking Missions. This report is the culmination of a two and one-half month review of preparations in Russia for the Phase 1A missions (Soyuz TM-21, Mir 18 Main Expedition, and STS-71). Once again the Task Force received tremendous support from many individuals and organizations at NASA. The same applied to our site visits in Russia where we were met with an openness and candor which served to reinforce our confidence in the ultimate success of the upcoming missions. Over the next two months, the Task Force will be focusing its efforts in two areas. The first are the preparations for STS-71, including the status of the Orbiter Docking System and the analysis of data produced by the STS-63 mission. The second area is the NASA and NASA contractor presence in Russia, including the interaction of Phase 1 and Phase 2 personnel, NASA and contractor functions, and the transition from Phase 1 to Phase 2. Sincerely, Thomas P. Stafford CC: NASA/HQ/Code A/Mr. Goldin NASA/HQ/Code A/Gen. Dailey NASA/HQ/Code A/Mr. -
Soviet Steps Toward Permanent Human Presence in Space
SALYUT: Soviet Steps Toward Permanent Human Presence in Space December 1983 NTIS order #PB84-181437 Recommended Citation: SALYUT: Soviet Steps Toward Permanent Human Presence in Space–A Technical Mere- orandum (Washington, D. C.: U.S. Congress, Office of Technology Assessment, OTA- TM-STI-14, December 1983). Library of Congress Catalog Card Number 83-600624 For sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402 Foreword As the other major spacefaring nation, the Soviet Union is a subject of interest to the American people and Congress in their deliberations concerning the future of U.S. space activities. In the course of an assessment of Civilian Space Stations, the Office of Technology Assessment (OTA) has undertaken a study of the presence of Soviets in space and their Salyut space stations, in order to provide Congress with an informed view of Soviet capabilities and intentions. The major element in this technical memorandum was a workshop held at OTA in December 1982: it was the first occasion when a significant number of experts in this area of Soviet space activities had met for extended unclassified discussion. As a result of the workshop, OTA prepared this technical memorandum, “Salyut: Soviet Steps Toward Permanent Human Presence in Space. ” It has been reviewed extensively by workshop participants and others familiar with Soviet space activities. Also in December 1982, OTA wrote to the U. S. S. R.’s Ambassador to the United States Anatoliy Dobrynin, requesting any information concerning present and future Soviet space activities that the Soviet Union judged could be of value to the OTA assess- ment of civilian space stations. -
Thesis Submitted to Florida Institute of Technology in Partial Fulfllment of the Requirements for the Degree Of
Dynamics of Spacecraft Orbital Refueling by Casey Clark Bachelor of Aerospace Engineering Mechanical & Aerospace Engineering College of Engineering 2016 A thesis submitted to Florida Institute of Technology in partial fulfllment of the requirements for the degree of Master of Science in Aerospace Engineering Melbourne, Florida July, 2018 ⃝c Copyright 2018 Casey Clark All Rights Reserved The author grants permission to make single copies. We the undersigned committee hereby approve the attached thesis Dynamics of Spacecraft Orbital Refueling by Casey Clark Dr. Tiauw Go, Sc.D. Associate Professor. Mechanical & Aerospace Engineering Committee Chair Dr. Jay Kovats, Ph.D. Associate Professor Mathematics Outside Committee Member Dr. Markus Wilde, Ph.D. Assistant Professor Mechanical & Aerospace Engineering Committee Member Dr. Hamid Hefazi, Ph.D. Professor and Department Head Mechanical & Aerospace Engineering ABSTRACT Title: Dynamics of Spacecraft Orbital Refueling Author: Casey Clark Major Advisor: Dr. Tiauw Go, Sc.D. A quantitative collation of relevant parameters for successfully completed exper- imental on-orbit fuid transfers and anticipated orbital refueling future missions is performed. The dynamics of connected satellites sustaining fuel transfer are derived by treating the connected spacecraft as a rigid body and including an in- ternal mass fow rate. An orbital refueling results in a time-varying local center of mass related to the connected spacecraft. This is accounted for by incorporating a constant mass fow rate in the inertia tensor. Simulations of the equations of motion are performed using the values of the parameters of authentic missions in an endeavor to provide conclusions regarding the efect of an internal mass transfer on the attitude of refueling spacecraft. -
Final Report of the International Space Station Independent Safety
I Contents Executive Summary........................................................................................ 1 Principal Observations ..................................................................................... 3 Principal Recommendations ............................................................................. 3 1. Introduction..................................................................................................... 5 Charter/Scope ................................................................................................... 5 Approach........................................................................................................... 5 Report Organization ......................................................................................... 5 2. The International Space Station Program.................................................... 7 International Space Station Characteristics..................................................... 8 3. International Space Station Crosscutting Management Functions............ 12 Robust On-Orbit Systems.................................................................................. 12 The Design ........................................................................................................ 12 Verification Requirements ................................................................................ 12 Physical (Fit) Verification ................................................................................ 13 Multi-element Integrated Test.......................................................................... -
Robotic Arm.Indd
Ages: 8-12 Topic: Engineering design and teamwork Standards: This activity is aligned to national standards in science, technology, health and mathematics. Mission X: Train Like an Astronaut Next Generation: 3-5-ETS1-2. Generate and compare multiple possible solutions to a problem based on how well each is likely A Robotic Arm to meet the criteria and constraints of the problem. 3-5-ETS1-3. Plan and carry out fair tests in which variables are controlled and failure points are considered to identify aspects of a model or prototype that can be EDUCATOR SECTION (PAGES 1-7) improved. STUDENT SECTION (PAGES 8-15) Background Why do we need robotic arms when working in space? As an example, try holding a book in your hands straight out in front of you and not moving them for one or two minutes. After a while, do your hands start to shake or move around? Imagine how hard it would be to hold your hands steady for many days in a row, or to lift something really heavy. Wouldn’t it be nice to have a really long arm that never gets tired? Well, to help out in space, scientists have designed and used robotic arms for years. On Earth, scientists have designed robotic arms for everything from moving heavy equipment to performing delicate surgery. Robotic arms are important machines that help people work on Earth as well as in space. Astronaut attached to a robotic arm on the ISS. Look at your arms once again. Your arms are covered in skin for protection. -
Orbital Fueling Architectures Leveraging Commercial Launch Vehicles for More Affordable Human Exploration
ORBITAL FUELING ARCHITECTURES LEVERAGING COMMERCIAL LAUNCH VEHICLES FOR MORE AFFORDABLE HUMAN EXPLORATION by DANIEL J TIFFIN Submitted in partial fulfillment of the requirements for the degree of: Master of Science Department of Mechanical and Aerospace Engineering CASE WESTERN RESERVE UNIVERSITY January, 2020 CASE WESTERN RESERVE UNIVERSITY SCHOOL OF GRADUATE STUDIES We hereby approve the thesis of DANIEL JOSEPH TIFFIN Candidate for the degree of Master of Science*. Committee Chair Paul Barnhart, PhD Committee Member Sunniva Collins, PhD Committee Member Yasuhiro Kamotani, PhD Date of Defense 21 November, 2019 *We also certify that written approval has been obtained for any proprietary material contained therein. 2 Table of Contents List of Tables................................................................................................................... 5 List of Figures ................................................................................................................. 6 List of Abbreviations ....................................................................................................... 8 1. Introduction and Background.................................................................................. 14 1.1 Human Exploration Campaigns ....................................................................... 21 1.1.1. Previous Mars Architectures ..................................................................... 21 1.1.2. Latest Mars Architecture ......................................................................... -
International Space Station Program Mobile Servicing System (MSS) To
SSP 42004 Revision E Mobile Servicing System (MSS) to User (Generic) Interface Control Document Part I International Space Station Program Revision E, May 22, 1997 Type 1 Approved by NASA National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No. NAS15–10000 SSP 42004, Part 1, Revision E May 22, 1997 REVISION AND HISTORY PAGE REV. DESCRIPTION PUB. DATE C Totally revised Space Station Freedom Document into an International Space Station Alpha Document 03–14–94 D Revision D reference PIRNs 42004–CS–0004A, 42004–NA–0002, 42004–NA–0003, TBD 42004–NA–0004, 42004–NA–0007D, 42004–NA–0008A, 42004–NA–0009C, 42004–NA–0010B, 42004–NA–0013A SSP 42004, Part 1, Revision E May 22, 1997 INTERNATIONAL SPACE STATION PROGRAM MOBILE SERVICING SYSTEM TO USER (GENERIC) INTERFACE CONTROL DOCUMENT MAY 22, 1997 CONCURRENCE PREPARED BY: PRINT NAME ORGN SIGNATURE DATE CHECKED BY: PRINT NAME ORGN SIGNATURE DATE SUPERVISED BY (BOEING): PRINT NAME ORGN SIGNATURE DATE SUPERVISED BY (NASA): PRINT NAME ORGN SIGNATURE DATE DQA: PRINT NAME ORGN SIGNATURE DATE i SSP 42004, Part 1, Revision E May 22, 1997 NASA/CSA INTERNATIONAL SPACE STATION PROGRAM MOBILE SERVICING SYSTEM (MSS) TO USER INTERFACE CONTROL DOCUMENT MAY 22, 1997 Print Name For NASA DATE Print Name For CSA DATE ii SSP 42004, Part 1, Revision E May 22, 1997 PREFACE SSP 42004, Mobile Servicing System (MSS) to User Interface Control Document (ICD) Part I shall be implemented on all new Program contractual and internal activities and shall be included in any existing contracts through contract changes. -
Tragic Tangle: Soyuz-1
National Aeronautics and Space Administration Tragic Tangle: Soyuz-1 Leadership ViTS Meeting June 2010 Bryan O’Connor Chief, Safety and Mission Assurance Wilson B. Harkins Deputy Chief, Safety and Mission Assurance This and previous presentations are archived at: sma.nasa.gov/safety-messages THE MISHAP On April 23,1967, the Soviet Union launched the Soyuz-1 spacecraft to achieve a new and elaborate docking capability. Multiple malfunctions on orbit forced ground crews to abort the mission. In a crippled spacecraft with rapidly draining power reserves, Cosmonaut Colonel Vladimir Komarov heroically maneuvered the craft for re-entry to Earth. Upon re-entry, the vehicle’s drag and backup parachutes entangled. With no means of braking, Soyuz-1 struck the ground at 90 miles per hour, and the USSR’s most experienced cosmonaut was killed. The Space Race Begins •1961-1963: The USSR flies six successful Vostok crewed missions. •1964-1966: No Soviet manned flights •1961-1966: The U.S. flies six crewed Mercury and ten crewed Gemini missions, pioneering techniques for use en route to the moon. Under immense pressure to overtake the Americans, the Soviets planned a 1967 mission involving two Soyuz spacecraft to rendezvous, dock, transfer cosmonauts, and commemorate May Day. Soyuz and Apollo Test Failures •November 1966: Kosmos-133 unmanned Soyuz suffers maneuvering problems upon re-entry and automatically self-destructs over the Pacific. • December 1966: Second unmanned Soyuz’ booster explodes on pad •January 1967: Apollo 204 fire kills three astronauts. • February 1967: Kosmos-140 unmanned Soyuz heat shield experiences 30mm burn-through during entry. •April 1967: Despite failures, as May Day approaches, Design Bureau Cosmonaut Colonel gives order for dual Soyuz mission. -
Gemini 6 Press
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION TELS. WO 2-4155 WASHINGTON, D.C. 20546 WO 3-6,925 FOR RELEASE: WEDNESDAY AM, S October 20, 1965 REUSE NO: 65-327 PROJECT: 6 CONTENTS Title Pa_e GENERAL NEWS RELEASE ........... '.......... 1-6 Orbits - Revolutions ...................... 7-10 Launch Vehicle Countdown .......... -....... ll-12 Experiments ............................... 13-I_ RadiationSynoptic Terrain...................Photography _ .................'.- 15,1b Synoptic Weather Photography ........... 17 Bio-Ch_mical Analysis of Body Fluids--- 17-18 70MMHasselblad Camera .................... 19 16MMMaurer Movie Camera .................. 20 Gemini 6 Nominal Maneuvers ................ 21 Checks while docked ....................... 22 Laser Beam0bservation .................... 23-24 Y_mmediate Preflight Crew Activities ....... 25-26 Mission Description ....................... 27-32 Manned Space Flight Tracking Network Gemini 6 Mission Requirements ........ 33 Tracking .................................. 34- 43 Network Configuration ..................... 44 Crew Safety ............................... _-47 Gemini Parachute Landing Sequence ......... 48 I AbortAtlanticProceduresRecovery..........................Area Communications ..... 49 Planned and Contingency Landing Areas ..... 50-51 Weather Requirements ...................... 52 Body Waste Disposal ....................... Gemini 6 Suit ............................. T FoodMedical.............Checks ............................"................ --- ..... 555_ WaherMen_s ...............Measuring -
Next Generation Advanced Video Guidance Sensor: Low Risk Rendezvous and Docking Sensor
Next Generation Advanced Video Guidance Sensor: Low Risk Rendezvous and Docking Sensor Jimmy Lee1 and Connie Carrington2 NASA Marshall Space Flight Center, Huntsville, AL, 35812 Susan Spencer3 NASA Marshall Space Flight Center, Huntsville, AL, 35812 and Thomas Bryan, Ricky T. Howard, Jimmie Johnson4 NASA Marshall Space Flight Center, Huntsville, AL, 35812 The Next Generation Advanced Video Guidance Sensor (NGAVGS) is being built and tested at MSFC. This paper provides an overview of current work on the NGAVGS, a summary of the video guidance heritage, and the AVGS performance on the Orbital Express mission. This paper also provides a discussion of applications to ISS cargo delivery vehicles, CEV, and future lunar applications. I. Introduction ELATIVE navigation sensors are an enabling technology for exploration vehicles such as the National R Aeronautics and Space Administration’s (NASA’s) Crew Exploration Vehicle (CEV), cargo vehicles for logistics delivery to the International Space Station (ISS), and lunar landers. Additional applications are lunar sample return missions, satellite servicing, and future on-orbit assembly of space structures. The Next Generation Advanced Video Guidance Sensor (NGAVGS) is a third generation relative navigation sensor that incorporates the basic functions developed and flight proven in the Advanced Video Guidance Sensor (AVGS). The AVGS was the primary proximity operations and docking sensor in the first autonomous docking in the history of the U.S. space program, which was accomplished on May 5, 2007 during the Orbital Express (OE) mission. However, the AVGS hardware cannot be reproduced due to parts obsolescence, which has provided Marshall Space Flight Center (MSFC) an opportunity to replace an obsolete imager and processor with radiation tolerant parts, and to address critical CEV and ISS cargo vehicle relative navigation sensor requirements. -
Launch Vehicle Classification for Decision-Making of Small
Trans. Japan Soc. Aero. Space Sci. Vol. 64, No. 4, pp. 234–241, 2021 DOI: 10.2322/tjsass.64.234 Launch Vehicle Classification for Decision-Making of Small Satellite Launch Options* Mengying ZHANG,1) Qin XU,2)† and Qingbin ZHANG1) 1)College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, Hunan 410073, China 2)Center for Assessment and Demonstration Research, Academy of Military Science, Beijing 100091, China In recent years, there has been a steady increase in the small satellite launch market. With the rapid development of novel launchers, for small satellite owners and operators, how to effectively and efficiently choose appropriate launch ve- hicles has become a major concern. Based on updated launch records, a reliable launch data source for multi-attribute eval- uation and reclassification is established. Using a statistical classification process, active launch vehicles are classified into five representative-in-class launchers on the basis of their capabilities and performance. Unlike the previous categorisation based on payload ability, this method captures launch cost, technology maturity, reliability and availability of each cat- egory within the current launch vehicles in service. Moreover, representatives are selected as the baseline types for the high-level planning and designing of complex small satellite launch missions. The analysis indicates that this study pro- vides a valid statistical classification and selection strategy of representative-in-class launch vehicles to support decision- making for rapid assessment on a large number of small satellite launch missions. Key Words: Small Satellite, Launcher Selection, Reliability, Launch Cost 1. Introduction 350 Small satellites (<=1000kg) 300 The past decade has witnessed a boom in the small satellite Large satellites (>1000kg) market. -
SOYUZ THROUGH the AGES the R-7 Rocket That Led to the Family of Soyuz Vehicles Launching Today Lifted Off for the First Time Onfeb
RUSSIAN SPACE SOYUZ THROUGH THE AGES The R-7 rocket that led to the family of Soyuz vehicles launching today lifted off for the first time onFeb. 17, 1959. The last launch, on Dec. 27, 2018, was number 1,898. Irene Klotz and Maxim Pyadushkin Vostochny Cosmodrome anufactured by the Progress Rocket Space Center in Sama- Evolution of Soyuz-Family Launch Vehicles ra, Russia, the medium-lift expendable booster originally was used for Soviet-era human space missions and later became the R-7 Soyuz Soyuz-L workhorse for the country’s civilian and military space programs. M 1957 First launch of the ICBM (SS-6 1966-76 (32 launches, 1970-71 (three launches, Sapwood) that served as a basis for including 30 successful, all successful, The first rocket officially named Soyuz was launched in Soviet/Russian launch vehicles from Baikonur) from Baikonur) 1966 and has since flown 1,050 times, of which 1,023 were including the Soyuz family successful. Production of Soyuz rockets peaked in the early Soyuz 1980s at about 60 vehicles per year. Medium-Class Launch Vehicle Russia began offering Soyuz launch services internationally in the mid-1980s through Glavkosmos, a commercial entity set up to sell Soviet rocket and space technologies. Manufacturer: Progress Rocket Space Soyuz-U/-U2 Soyuz-M Center, Samara, Russia In 1996, Russia created Starsem, a joint venture (35% ArianeGroup, 25% Roscosmos, 25% RKTs Progress, 15% 1991 Breakup of the 1973-2017 1971-76 (eight launches, Soviet Union, (859 launches, including all successful, from Plesetsk) Dimensions Arianespace) that had exclusive rights to provide commercial launch services on Soyuz launch vehicles.