Crusan Evolvable Mars Campaign and Technology Development
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Flight Opportunities and Small Spacecraft Technology Program Updates NAC Technology, Innovation and Engineering Committee Meeting | March 19, 2020
Flight Opportunities and Small Spacecraft Technology Program Updates NAC Technology, Innovation and Engineering Committee Meeting | March 19, 2020 Christopher Baker NASA Space Technology Mission Directorate Flight Opportunities and Small Spacecraft Technology Program Executive National Aeronautics and Space Administration 1 CHANGING THE PACE OF SPACE Through Small Spacecraft Technology and Flight Opportunities, Space Tech is pursuing the rapid identification, development, and testing of capabilities that exploit agile spacecraft platforms and responsive launch capabilities to increase the pace of space exploration, discovery, and the expansion of space commerce. National Aeronautics and Space Administration 2 THROUGH SUBORBITAL FLIGHT The Flight Opportunities program facilitates rapid demonstration of promising technologies for space exploration, discovery, and the expansion of space commerce through suborbital testing with industry flight providers LEARN MORE: WWW.NASA.GOV/TECHNOLOGY Photo Credit: Blue Origin National Aeronautics and Space Administration 3 FLIGHT OPPORTUNITIES BY THE NUMBERS Between 2011 and today… In 2019 alone… Supported 195 successful fights Supported 15 successful fights Enabled 676 tests of payloads Enabled 47 tests of payloads 254 technologies in the portfolio 86 technologies in the portfolio 13 active commercial providers 9 active commercial providers National Aeronautics and Space Administration Numbers current as of March 1, 2020 4 TECHNOLOGY TESTED IN SUBORBITAL Lunar Payloads ISS SPACE IS GOING TO EARTH ORBIT, THE MOON, MARS, AND BEYOND Mars 2020 Commercial Critical Space Lunar Payload Exploration Services Solutions National Aeronautics and Space Administration 5 SUBORBITAL INFUSION HIGHLIGHT Commercial Lunar Payload Services Four companies selected as Commercial Lunar Payload Services (CPLS) providers leveraged Flight Opportunities-supported suborbital flights to test technologies that are incorporated into their landers and/or are testing lunar landing technologies under Flight Opportunities for others. -
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 -
Hearing Transcript
The President’s Commission on Implementation of United States Space Exploration Policy PUBLIC HEARING Georgia Centers for Advanced Telecommunications Technology 250 14th Street, NW Atlanta, GA Wednesday, March 24, and Thursday, March 25, 2004 Pete Aldridge Well, good afternoon. I’m Pete Aldridge, I’m the Chairman of the President’s Commission on the Implementation of the U.S. Space Exploration Policy, or as I have shortened it, the “President’s Commission on the Moon, Mars, and Beyond.” I was delighted when I learned that Monica Scarbrough, the Director of Development, invited us here. The Georgia Institute of Technology is in fact my alma mater, and it’s generally great to be back on campus. I’m looking forward to looking around at some of the old haunts that I spent many hours on. The Commission is here to explore ways to achieve the President’s vision of going back to the Moon and on to Mars and beyond. We have listened, we’ve talked to experts at two previous hearings—in Washington, D.C., and in Dayton, Ohio. We’ve talked among ourselves and we realized this vision provides a focus not just for NASA, but a focus that can revitalize U.S. space capability and have a significant impact upon our nation’s industrial base and academia. As you can see from our agenda, we are talking with experts from many, many disciplines, including those outside the traditional aerospace arena. Before I go any further, let me introduce my fellow Commissioners. And begin on the audience’s right, Carly Fiorina. -
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.......................................................................... -
Highlights in Space 2010
International Astronautical Federation Committee on Space Research International Institute of Space Law 94 bis, Avenue de Suffren c/o CNES 94 bis, Avenue de Suffren UNITED NATIONS 75015 Paris, France 2 place Maurice Quentin 75015 Paris, France Tel: +33 1 45 67 42 60 Fax: +33 1 42 73 21 20 Tel. + 33 1 44 76 75 10 E-mail: : [email protected] E-mail: [email protected] Fax. + 33 1 44 76 74 37 URL: www.iislweb.com OFFICE FOR OUTER SPACE AFFAIRS URL: www.iafastro.com E-mail: [email protected] URL : http://cosparhq.cnes.fr Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law The United Nations Office for Outer Space Affairs is responsible for promoting international cooperation in the peaceful uses of outer space and assisting developing countries in using space science and technology. United Nations Office for Outer Space Affairs P. O. Box 500, 1400 Vienna, Austria Tel: (+43-1) 26060-4950 Fax: (+43-1) 26060-5830 E-mail: [email protected] URL: www.unoosa.org United Nations publication Printed in Austria USD 15 Sales No. E.11.I.3 ISBN 978-92-1-101236-1 ST/SPACE/57 *1180239* V.11-80239—January 2011—775 UNITED NATIONS OFFICE FOR OUTER SPACE AFFAIRS UNITED NATIONS OFFICE AT VIENNA Highlights in Space 2010 Prepared in cooperation with the International Astronautical Federation, the Committee on Space Research and the International Institute of Space Law Progress in space science, technology and applications, international cooperation and space law UNITED NATIONS New York, 2011 UniTEd NationS PUblication Sales no. -
For Immediate Release: TWO GOOGLE LUNAR XPRIZE
Media Contact: Kyoko Yonezawa [email protected] For Immediate Release: TWO GOOGLE LUNAR XPRIZE TEAMS ANNOUNCE RIDESHARE PARTNERSHIP FOR MISSION TO THE MOON IN 2016 Team HAKUTO (Japan) and Team Astrobotic (U.S.) Plan Cooperative Launch in Pursuit of $30 Million Prize to Land a Private Spacecraft on the Lunar Surface TOKYO, Japan (February 24, 2015) – HAKUTO, the only Japanese team competing for the $30 million Google Lunar XPRIZE, has announced a contract with fellow competitor, Astrobotic, based in Pittsburgh, Pa., to carry a pair of rovers to the moon. Astrobotic plans to launch its Google Lunar XPRIZE mission on a SpaceX Falcon 9 rocket from Cape Canaveral, Fla., during the second half of 2016. HAKUTO’s twin rovers, Moonraker and Tetris, will piggyback on Astrobotic's Griffin lander to reach the lunar surface. Upon touchdown, the rovers will be released simultaneously with Astrobotic’s Andy rover, developed by Carnegie Mellon University, travel 500 meters on the moon’s surface and send high-definition images and video back to Earth, all in pursuit of the $20M Google Lunar XPRIZE Grand Prize. Last month, both teams were awarded Google Lunar XPRIZE Milestone Prizes: HAKUTO won $500,000 for technological advancements in the Mobility category, while Astrobotic, in partnership with Carnegie Mellon University, won a total of $1.75M for innovations in all three focus areas—Landing, Mobility and Imaging. Throughout the judging process, all three rovers, Moonraker, Tetris and Andy, demonstrated the ability to move 500 meters across the lunar surface and withstand the high radiation environment and extreme temperatures on the moon. -
Space Act Agreement Between the National Aeronautics and Space Administration and Moon Express Inc. for Lunar Catalyst Article 1
SPACE ACT AGREEMENT BETWEEN THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION AND MOON EXPRESS INC. FOR LUNAR CATALYST ARTICLE 1. AUTHORITY AND PARTIES In accordance with the National Aeronautics and Space Act (51 U.S.C. § 20113), this Agreement is entered into by the National Aeronautics and Space Administration, located at 300 E Street SW, Washington, DC 20546 (hereinafter referred to as "NASA") and Moon Express, Inc. located at 100 Space Port Way, Cape Canaveral, Florida 32920 (hereinafter referred to as "Partner" or "Moon Express"). NASA and Partner may be individually referred to as a "Party" and collectively referred to as the "Parties." ARTICLE 2. PURPOSE This agreement is an amended version of Space Act Agreement #18251, which went into effect on September 30, 2014. NASA recognizes that private-sector investment in technologies intended to enable commercial lunar activities has been increasing. In addition to recognizing these activities NASA wants to encourage and enable commercial successes to cultivate the increased innovation and entrepreneurship in the commercial space transportation sector. The “Lunar Cargo Transportation and Landing by Soft Touchdown” (Lunar CATALYST) initiative, is consistent with the National Space Transportation Policy. Per this policy, NASA is “committed to encouraging and facilitating a viable, healthy, and competitive U.S. Commercial space transportation industry”. This initiative also supports the internationally shared space exploration goals of the Global Exploration Roadmap (GER) that NASA and 11 other space agencies around the world released in August 2013. The GER acknowledges the value of public-private partnerships and commercial services to enable sustainable exploration of asteroids, the Moon and Mars. -
Habitation Module 26 July 2016 – NASA Advisory Council, Human Exploration and Operations Committee
National Aeronautics and Space Administration Habitation Module 26 July 2016 – NASA Advisory Council, Human Exploration and Operations Committee Jason Crusan | Advanced Exploration Systems Director | NASA Headquarters 2 Human Exploration of Mars Is Hard Common Capability Needs Identified from Multiple Studies Days Reliable In-Space 800-1,100 44 min Transportation Total me crew is Maximum two- away from Earth – way communicaon for orbit missions all in 2me delay – 300 KW Micro-g and Radia2on Autonomous Opera2ons Total connuous transportaon power 130 t Heavy-LiA Mass 20-30 t Long Surface Stay Multiple Ability to 500 Days Launches per land large mission payloads Surface Operations Dust Toxicity and 100 km 11.2 km/s Long Range Explora2on Earth Entry Speed 20 t Oxygen produced for ascent to orbit - ISRU 3 The Habitation Development Challenge HABITATATION CAPABILITY Days 800-1,100 Habitation Systems – Total me crew is AES/ISS/STMD away from Earth – • Environmental Control & Life Support for orbit missions all in • Autonomous Systems Micro-g and Radia2on Integrated • EVA testing on ISS • Fire Safety • Radiation Protection Habitation Systems - Crew Health – HRP Long Surface Stay • Human Research 500 Days • Human Performance • Exercise PROVING GROUND Validation in cislunar space • Nutrition Habitation Capability– NextSTEP BAA / Int. Partners • Studies and ground prototypes of pressurized volumes 4 Specific Habitation Systems Objectives TODAY FUTURE Habitation The systems, tools, and protec:ons that allow Systems Elements humans to live and work -
NVIDIA Maximus Success Story NVIDIA Maximus Technology Helps Astrobotic Ignite New Era of Moon Exploration When the Google Luna
NVIDIA Maximus Success Story NVIDIA Maximus Technology Helps Astrobotic Ignite New Era of Moon Exploration When the Google Lunar X PRIZE was announced in 2010, Astrobotic Technology was among the first to heed the call. The reward: a total of $30 million, the largest international incentive prize of all time, available to privately funded teams. The challenge: be the first to safely land a robot on the surface of the moon, control the robot to travel 500 meters over the lunar surface, and send high-definition (HD) video, images, and data back to earth. “Astrobotic is a bit like UPS, but for the moon,” said Jason Calaiaro, director of Information Systems for Astrobotic Technology. The company’s primary service is the delivery of payloads – scientific instruments, space agency exploration gear, data collection devices, etc. – to the lunar surface. The Lunar X PRIZE fit nicely with Astrobotic’s goals and business model and promises to provide some high-profile publicity to the company. To help keep its competitive dreams on track, Astrobotic needed to be able to do its complex robot design, structural and vibration analysis, and visualization more quickly and completely. The company upgraded its hardware to include NVIDIA® Maximus™ technology powering Dassault Systèmes SolidWorks, ANSYS, and MathWorks MATLAB software. Not only is this sophisticated technology helping position Astrobotic for Lunar X success, it is also helping to ramp up the company’s main commercial ventures. CHALLENGE Astrobotic was founded in 2008 as a spin-off from the Robotics Institute of Carnegie Mellon University in Pittsburgh, PA, with the mission to build robots able to explore and deliver payloads to the moon, Mars, and beyond. -
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. -
KPLO, ISECG, Et Al…
NationalNational Aeronautics Aeronautics and Space and Administration Space Administration KPLO, ISECG, et al… Ben Bussey Chief Exploration Scientist Human Exploration & Operations Mission Directorate, NASA HQ 1 Strategic Knowledge Gaps • SKGs define information that is useful/mandatory for designing human spaceflight architecture • Perception is that SKGs HAVE to be closed before we can go to a destination, i.e. they represent Requirements • In reality, there is very little information that is a MUST HAVE before we go somewhere with humans. What SKGs do is buy down risk, allowing you to design simpler/cheaper systems. • There are three flavors of SKGs 1. Have to have – Requirements 2. Buys down risk – LM foot pads 3. Mission enhancing – Resources • Four sets of SKGs – Moon, Phobos & Deimos, Mars, NEOs www.nasa.gov/exploration/library/skg.html 2 EM-1 Secondary Payloads 13 CUBESATS SELECTED TO FLY ON INTERIM EM-1 CRYOGENIC PROPULSION • Lunar Flashlight STAGE • Near Earth Asteroid Scout • Bio Sentinel • LunaH-MAP • CuSPP • Lunar IceCube • LunIR • EQUULEUS (JAXA) • OMOTENASHI (JAXA) • ArgoMoon (ESA) • STMD Centennial Challenge Winners 3 3 3 Lunar Flashlight Overview Looking for surface ice deposits and identifying favorable locations for in-situ utilization in lunar south pole cold traps Measurement Approach: • Lasers in 4 different near-IR bands illuminate the lunar surface with a 3° beam (1 km spot). Orbit: • Light reflected off the lunar • Elliptical: 20-9,000 km surface enters the spectrometer to • Orbit Period: 12 hrs distinguish water