The International Space Station
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A Feasibility Study for Using Commercial Off the Shelf (COTS)
University of Tennessee, Knoxville TRACE: Tennessee Research and Creative Exchange Masters Theses Graduate School 8-2011 A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2 Chad Lee Davis University of Tennessee - Knoxville, [email protected] Follow this and additional works at: https://trace.tennessee.edu/utk_gradthes Part of the Aerodynamics and Fluid Mechanics Commons, Other Aerospace Engineering Commons, and the Space Vehicles Commons Recommended Citation Davis, Chad Lee, "A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2. " Master's Thesis, University of Tennessee, 2011. https://trace.tennessee.edu/utk_gradthes/965 This Thesis is brought to you for free and open access by the Graduate School at TRACE: Tennessee Research and Creative Exchange. It has been accepted for inclusion in Masters Theses by an authorized administrator of TRACE: Tennessee Research and Creative Exchange. For more information, please contact [email protected]. To the Graduate Council: I am submitting herewith a thesis written by Chad Lee Davis entitled "A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2." I have examined the final electronic copy of this thesis for form and content and recommend that it be accepted in partial fulfillment of the equirr ements for the degree of Master of Science, with a major in Aerospace Engineering. -
Development of the Crew Dragon ECLSS
ICES-2020-333 Development of the Crew Dragon ECLSS Jason Silverman1, Andrew Irby2, and Theodore Agerton3 Space Exploration Technologies, Hawthorne, California, 90250 SpaceX designed the Crew Dragon spacecraft to be the safest ever flown and to restore the ability of the United States to launch astronauts. One of the key systems required for human flight is the Environmental Control and Life Support System (ECLSS), which was designed to work in concert with the spacesuit and spacecraft. The tight coupling of many subsystems combined with an emphasis on simplicity and fault tolerance created unique challenges and opportunities for the design team. During the development of the crew ECLSS, the Dragon 1 cargo spacecraft flew with a simple ECLSS for animals, providing an opportunity for technology development and the early characterization of system-level behavior. As the ECLSS design matured a series of tests were conducted, including with humans in a prototype capsule in November 2016, the Demo-1 test flight to the ISS in March 2019, and human-in-the-loop ground testing in the Demo-2 capsule in January 2020 before the same vehicle performs a crewed test flight. This paper describes the design and operations of the ECLSS, the development process, and the lessons learned. Nomenclature AC = air conditioning AQM = air quality monitor AVV = active vent valve CCiCap = Commercial Crew Integrated Capability CCtCap = Commercial Crew Transportation Capability CFD = computational fluid dynamics conops = concept of operations COPV = composite overwrapped -
The International Space Station and the Space Shuttle
Order Code RL33568 The International Space Station and the Space Shuttle Updated November 9, 2007 Carl E. Behrens Specialist in Energy Policy Resources, Science, and Industry Division The International Space Station and the Space Shuttle Summary The International Space Station (ISS) program began in 1993, with Russia joining the United States, Europe, Japan, and Canada. Crews have occupied ISS on a 4-6 month rotating basis since November 2000. The U.S. Space Shuttle, which first flew in April 1981, has been the major vehicle taking crews and cargo back and forth to ISS, but the shuttle system has encountered difficulties since the Columbia disaster in 2003. Russian Soyuz spacecraft are also used to take crews to and from ISS, and Russian Progress spacecraft deliver cargo, but cannot return anything to Earth, since they are not designed to survive reentry into the Earth’s atmosphere. A Soyuz is always attached to the station as a lifeboat in case of an emergency. President Bush, prompted in part by the Columbia tragedy, made a major space policy address on January 14, 2004, directing NASA to focus its activities on returning humans to the Moon and someday sending them to Mars. Included in this “Vision for Space Exploration” is a plan to retire the space shuttle in 2010. The President said the United States would fulfill its commitments to its space station partners, but the details of how to accomplish that without the shuttle were not announced. The shuttle Discovery was launched on July 4, 2006, and returned safely to Earth on July 17. -
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.......................................................................... -
Spaceport News Pioneering the Future America's Gateway to the Universe
May 14, 1999 Vol. 38, No. 10 Fortieth Anniversary Spaceport News Pioneering the Future America's gateway to the universe. Leading the world in preparing and launching missions to Earth and beyond. John F. Kennedy Space Center Preparing GOES to go Packing up for a trip to the space station Packing li ght isn't an option for the seven-member crew of STS-96, scheduled to lift off to the Inter national Space Station (ISS) on May 20 from Kennedy Space Center's Launch Pad 39B. The 10-day flight will take about two tons of supplies - including laptop computers, a printer, cameras, maintenance tools, spare parts and clothing- to the orbiting space station in the SPACEHAB double module. Discovery will be the first orbiter to dock with the fledgling station since the crew of Endeavour departed the outpost in December 1998. At Astrotech in Titusville, STS-96 will also be the first Fla., the GOES-L weather logistics flight to the new station. satellite was encapsulated in Discovery will spend five days its fairing before transfer to linked to the ISS, transferring and Launch Pad 36B at Cape installing gear that could not be Canaveral Air Station. The fourth of a new (See STS-96, Page 5) advanced series of geo At left, In the payload changeout room at stationary weather satellites Launch Pad 39B, technicians moved the for the National Oceanic and SPACEHAB double module from the payload canister on April 28 and placed it Atmospheric Administration in Space Shuttle Discovery's payload bay (NOAA), GOES-Lis a three for STS-96. -
Glex-2021 – 6.1.1
Global Space Exploration Conference (GLEX 2021), St Petersburg, Russian Federation, 14-18 June 2021. Copyright ©2021 by Christophe Bonnal (CNES). All rights reserved. GLEX-2021 – 6.1.1 Human spaceflight from Guiana Space Center Ch. Bonnal1* – J-M. Bahu1 – Ph. Berthe2 – J. Bertrand1 – Ch. Bonhomme1 – M. Caporicci2 J-F. Clervoy3 – N. Costedoat4 – E. Coletti5 – G. Collange5 – G. Debas5 – R. Delage6 – J. Droz5 E. Louaas1 – P. Marx8 – B. Muller6 – S. Perezzan1 – I. Quinquis5 – S. Sandrone7 D. Schmitt2 – V. Taponier1 1 CNES Launcher Directorate, Pairs, France – 2 ESA Human & Robotic Exploration Directorate, ESTEC, Noordwijk, Netherlands – 3 Astronaut Novespace, Paris, France – 4CNES Guiana Space Center, Kourou, France 5ArianeGroup, Les Mureaux, France – 6Airbus Defence & Space, Toulouse, France – 7Airbus Defence & Space, Bremen Germany – 8Consultant, Paris, France * Corresponding Author Abstract The use of Space has drastically evolved these last ten years. Tomorrow will see easier and cheaper access to Space, satellite servicing, in-orbit manufacturing, human private spaceflights to ever increasing number of Orbital Stations, road to the Moon, Asteroids, Mars. It seems fundamental to make sure we can rely on robust, reliable, frequent and affordable access to and from LEO with both automatic systems and human missions; such systems are the bricks with which all the future operations in Space will be built. Independent human access to space from Europe for our astronauts is a key to any future in Space. It has been studied in depth since the 80's with Hermes Spaceplane, then through numerous studies, pre- development activities, and demonstrations such as ARD, X38-CRV or IXV, which now allow Europe to reconsider such an endeavor with a much higher confidence. -
Observations of the Performance of the U.S. Laboratory Architecture
---------------~ Source of Acqui sition NAS A Johnson Space Center Observations of the performance of the U.S. Laboratory Architecture Rod Jones National Aeronautics and Space Adm inistration , Lyndon B. Johnson Space Center ABSTRACT Station " 2000-01-2329 described the requirements selection process used to define the quadrant or The United States Laboratory Module "Destiny" was four post architecture of the Space Station the product of many architectural, technology, pressurized elements. The key features where the manufacturing, schedule and cost constraints pressure vessel envelope, standoffs, racks and which spanned 15 years. Requirements for the hatch shape and size. Space Station pressurized elements were developed and baselined in the mid to late '80's. Although the station program went through several design changes the fundamental requirements that drove the architecture did not change. Manufacturing of the U.S. Laboratory began in the early 90's. Final assembly and checkout testing completed in December of 2000. Destiny was launched, mated to the International Space Station and successfully activated on the STS-98 mission in February of 2001. The purpose of this paper is to identify key requirements, which directly or indirectly established the architecture of the U.S. Laboratory. Provide an overview of how that architecture affected the manufacture, assembly, test, and activation of the module on-orbit. And finally, through observations made during the last year of operation, provide considerations in the development of future requirements and mission integration controls for space habitats. ARCHITECTURE AND REQUIREMENTS In normal building construction the product of "architecture" are the drawings and specifications, which identify hardware requ irements and depict the integrated design. -
The New American Space Age: a Progress Report on Human Spaceflight the New American Space Age: a Progress Report on Human Spaceflight the International Space
The New American Space Age: A PROGRESS REPORT ON HUMAN SpaCEFLIGHT The New American Space Age: A Progress Report on Human Spaceflight The International Space Station: the largest international scientific and engineering achievement in human history. The New American Space Age: A Progress Report on Human Spaceflight Lately, it seems the public cannot get enough of space! The recent hit movie “Gravity” not only won 7 Academy Awards – it was a runaway box office success, no doubt inspiring young future scientists, engineers and mathematicians just as “2001: A Space Odyssey” did more than 40 years ago. “Cosmos,” a PBS series on the origins of the universe from the 1980s, has been updated to include the latest discoveries – and funded by a major television network in primetime. And let’s not forget the terrific online videos of science experiments from former International Space Station Commander Chris Hadfield that were viewed by millions of people online. Clearly, the American public is eager to carry the torch of space exploration again. Thankfully, NASA and the space industry are building a host of new vehicles that will do just that. American industry is hard at work developing new commercial transportation services to suborbital altitudes and even low Earth orbit. NASA and the space industry are also building vehicles to take astronauts beyond low Earth orbit for the first time since the Apollo program. Meanwhile, in the U.S. National Lab on the space station, unprecedented research in zero-g is paving the way for Earth breakthroughs in genetics, gerontology, new vaccines and much more. -
STS-129 Stocking the Station PRESS KIT/November 2009
National Aeronautics and Space Administration SPACE SHUTTLE MISSION STS-129 Stocking the Station www.nasa.gov www.nasa.gov PRESS KIT/November 2009 CONTENTS Section Page STS-129/ULF-3 MISSION OVERVIEW .................................................................................... 1 STS-129 TIMELINE OVERVIEW ............................................................................................... 9 MISSION PROFILE ................................................................................................................... 11 MISSION OBJECTIVES ............................................................................................................ 13 MISSION PERSONNEL ............................................................................................................. 15 STS-129 CREW ....................................................................................................................... 17 PAYLOAD OVERVIEW .............................................................................................................. 27 S-BAND ANTENNA SUPPORT ASSEMBLY (SASA) AND RADIO FREQUENCY GROUP (RFG) ..................... 29 EXPRESS LOGISTICS CARRIER 1 AND 2 ............................................................................................... 31 RENDEZVOUS & DOCKING ....................................................................................................... 47 UNDOCKING, SEPARATION, AND DEPARTURE ...................................................................................... 48 SPACEWALKS -
Please Type Your Paper Title Here In
Estimating the Reliability of a Soyuz Spacecraft Mission Michael G. Lutomskia*, Steven J. Farnham IIb, and Warren C. Grantb aNASA-JSC, Houston, TX – [email protected] bARES Corporation, Houston, TX Abstract: Once the US Space Shuttle retires in 2010, the Russian Soyuz Launcher and Soyuz Spacecraft will comprise the only means for crew transportation to and from the International Space Station (ISS). The U.S. Government and NASA have contracted for crew transportation services to the ISS with Russia. The resulting implications for the US space program including issues such as astronaut safety must be carefully considered. Are the astronauts and cosmonauts safer on the Soyuz than the Space Shuttle system? Is the Soyuz launch system more robust than the Space Shuttle? Is it safer to continue to fly the 30 year old Shuttle fleet for crew transportation and cargo resupply than the Soyuz? Should we extend the life of the Shuttle Program? How does the development of the Orion/Ares crew transportation system affect these decisions? The Soyuz launcher has been in operation for over 40 years. There have been only two loss of life incidents and two loss of mission incidents. Given that the most recent incident took place in 1983, how do we determine current reliability of the system? Do failures of unmanned Soyuz rockets impact the reliability of the currently operational man-rated launcher? Does the Soyuz exhibit characteristics that demonstrate reliability growth and how would that be reflected in future estimates of success? NASA’s next manned rocket and spacecraft development project is currently underway. -
Fachprogramme Raumfahrt
Fachprogramme Raumfahrt Aktualisierung 2002/2003 Raumfahrtmanagement Herausgeber: Deutsches Zentrum für Luft- und Raumfahrt e.V. Raumfahrtmanagement Königswinterer Str. 522 – 524 53227 Bonn-Oberkassel Fachprogramme Raumfahrt Aktualisierung 2002/2003 Gliederung TEIL 1 - ALLGEMEINE ASPEKTE 1. PROGRAMMRAHMEN UND -UMFELD .................................................................................... 5 2. STRUKTUR UND MITTELEINSATZ ........................................................................................... 6 TEIL 2 - FACHPROGRAMME EINFÜHRUNG................................................................................................................... 11 1. FACHPROGRAMM KOMMUNIKATION .................................................................................... 13 2. FACHPROGRAMM NAVIGATION .......................................................................................... 23 3. FACHPROGRAMM ERDBEOBACHTUNG .................................................................................. 31 4. FACHPROGRAMM ERFORSCHUNG DES WELTRAUMS................................................................. 43 5. FACHPROGRAMM FORSCHUNG UNTER WELTRAUMBEDINGUNGEN............................................... 55 6. FACHPROGRAMM RAUMSTATION ........................................................................................ 69 7. FACHPROGRAMM RAUMTRANSPORT .................................................................................... 79 8. FACHPROGRAMM TECHNIK FÜR RAUMFAHRTSYSTEME............................................................. -
Developing the Space Shuttle1
****EU4 Chap 2 (161-192) 4/2/01 12:45 PM Page 161 Chapter Two Developing the Space Shuttle1 by Ray A. Williamson Early Concepts of a Reusable Launch Vehicle Spaceflight advocates have long dreamed of building reusable launchers because they offer relative operational simplicity and the potential of significantly reduced costs com- pared to expendable vehicles. However, they are also technologically much more difficult to achieve. German experimenters were the first to examine seriously what developing a reusable launch vehicle (RLV) might require. During the 1920s and 1930s, they argued the advantages and disadvantages of space transportation, but were far from having the technology to realize their dreams. Austrian engineer Eugen M. Sänger, for example, envi- sioned a rocket-powered bomber that would be launched from a rocket sled in Germany at a staging velocity of Mach 1.5. It would burn rocket fuel to propel it to Mach 10, then skip across the upper reaches of the atmosphere and drop a bomb on New York City. The high-flying vehicle would then continue to skip across the top of the atmosphere to land again near its takeoff point. This idea was never picked up by the German air force, but Sänger revived a civilian version of it after the war. In 1963, he proposed a two-stage vehi- cle in which a large aircraft booster would accelerate to supersonic speeds, carrying a rel- atively small RLV to high altitudes, where it would be launched into low-Earth orbit (LEO).2 Although his idea was advocated by Eurospace, the industrial consortium formed to promote the development of space activities, it was not seriously pursued until the mid- 1980s, when Dornier and other German companies began to explore the concept, only to drop it later as too expensive and technically risky.3 As Sänger’s concepts clearly illustrated, technological developments from several dif- ferent disciplines must converge to make an RLV feasible.