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. -
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. -
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. -
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. -
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 -
Internationale Raumstation ISS International Space Station ISS
Internationale Raumstation ISS International Space Station ISS www.DLR.de Europäisches Labormodul COLUMBUS European laboratory module COLUMBUS US-Labormodul DESTINY japanisches Labormodul KIBO US laboratory module DESTINY Japanese laboratory module KIBO Russisches Cargo-Modul SaRja (Functional Cargo Block) Russian cargo module ZARYA 20. November 1998: (Functional Cargo Block) 24. Februar 2011: Start des ersten ISS-Moduls: Start des permanenten der Functional Cargo Block Logistikmoduls PMM (FGB) Sarja Leonardo November 20, 1998: February 24, 2011: launch of the first ISS module: launch of the logistic the Functional Cargo Block module PMM Leonardo (FGB) Zarya 12. juli 2000: 8. Februar 2010: Start des Service- und Wohn- Start des Aussichtsmoduls moduls Swesda Cupola July 12, 2000: February 8, 2011: launch of the observatory launch of the service and Russisches Service-Modul habitation module Zvezda module Cupola SwESDa Russian service module 10. November 2009: 7. Februar 2001: Europäisches Logistikmodul aTV-2 Start des amerikanischen ZvEZDA Start des russischen Docking- Labormoduls DESTINY (automated Transfer Vehicle) moduls POISK Mini-Research „johannes Kepler“ Module 2 February 7, 2001: 7. Februar 2008: 31. Mai 2008: launch of the American European logistics module ATv-2 November 10, 2009: Start des europäischen Start des zweiten Teils des laboratory module DESTINY (Automated Transfer vehicle) launch of the Russian docking Labormoduls japanischen Labormoduls “Johannes Kepler” module POISK Mini-Research COLUMBUS KIBO Pressurized Module (PM) Module 2 February 7, 2008: May 31, 2008: launch of the European launch of the second part of the research module Japanese laboratory module KIBO COLUMBUS Pressurized Module (PM) ISS ISS © NASA, ESA, DLR Forschung im All für die Menschen auf der Erde Research in Space for Mankind on Earth. -
Space Station Freedom. a Foothold on the Future. INSTITUTION National Aeronautics and Space Administration, Washington, DC
DOCUMENT RESUME ED 310 939 SE 050 885 AUTHOR David, Leonard TITLE Space Station Freedom. A Foothold on the Future. INSTITUTION National Aeronautics and Space Administration, Washington, DC. Office of Space Sta.:Ion. REPORT NO NP-107/10-88 PUB DATE 89 NOTE 49p.; Colored photographs and drawings may not reproduce well. PUB TYPE Reports - Descriptive (141) EDRS PRICE MF01/PCO2 Plus Postage. DESCRIPTORS *Aerospace Technology; Engineering Technology; Planning; *Satellites (Aerospace); Science Materials; *Science Programs; *Scientific Research; *Space Exploration; *Space Sciences IDENTIFIERS *Space Station ABSTRACT This booklet describes the planning of the space station program. Sections included are: (1) "Introduction"; (2) "A New Era Begins" (discussing scientific experiments on the space station); (3) "Living in Space";(4) "Dreams Fulfilled" (summarizing the history of the space station development, including the skylab and shuttle); (5) "Building a Way Station to Worlds Beyond" (illustrating an approach to building the space station); (6) ''Orbital Mechanics" (discussing the maneuverability of the space station, including robotic application);(7) "Evolving with Versatility" (describing blueprints for expanding a space station); and (8) "Foothold on the Future" (discussing the future plans of the space station program). (YP) **************************************-******************************* * Reproductions supplied by EDRS are the best that can be made * from the original document. *********************************************************************A* -
Analysis of Illumination Conditions at the Lunar South Pole Using Parallel Computing Techniques
Technische Universitat¨ Berlin Master Thesis Analysis of illumination conditions at the lunar south pole using parallel computing techniques Supervisors: Author: Dipl.-Ing. Philipp Glaser¨ Ramiro Marco figuera Prof. Dr. J¨urgen Oberst A thesis submitted in fulfilment of the requirements for the degree of Master of Science in the Planetary Geodesy Research Group Department of Geodesy and Geoinformation Science November 2014 Declaration of Authorship I, Ramiro Marco figuera, declare that this thesis titled, 'Analysis of illumination conditions at the lunar south pole using parallel computing techniques' and the work presented in it are my own. I confirm that: This work was done wholly or mainly while in candidature for a research degree at this University. Where any part of this thesis has previously been submitted for a degree or any other qualification at this University or any other institution, this has been clearly stated. Where I have consulted the published work of others, this is always clearly at- tributed. Where I have quoted from the work of others, the source is always given. With the exception of such quotations, this thesis is entirely my own work. I have acknowledged all main sources of help. Where the thesis is based on work done by myself jointly with others, I have made clear exactly what was done by others and what I have contributed myself. Signed: Date: i TECHNISCHE UNIVERSITAT¨ BERLIN Abstract Faculty VI Planning - Building - Environment Department of Geodesy and Geoinformation Science Master of Science Analysis of illumination conditions at the lunar south pole using parallel computing techniques by Ramiro Marco figuera In this Master Thesis an analysis of illumination conditions at the lunar south pole using parallel computing techniques is presented. -
Orb2: Spherical Space Station Designed for Single Launch and On-Orbit Assembly
Orb2: Spherical Space Station Designed for Single Launch and On-Orbit Assembly Vojtech Holub ∗ Unaffiliated With upcoming heavy and super-heavy lift rockets targeted for launch in 2021, a new class of payloads can be launched into low Earth orbit. This paper presents a design for a space station capable of being lifted by a single Blue Origin New Glenn vehicle. Once assembled on-orbit, it contains more than twice the pressurized volume of the International Space Station. The pressurized volume of traditional space station modules is limited by the dimensions of the payload fairing. The proposed Orb2 design consists of a spherical habitation module and a service module. The habitation module avoids the volume limitation by being launched in a flat-packed stack and assembled and welded robotically in orbit. Using CAD and finite element analysis, this paper shows that the habitation module contains approximately 2000 m3 of pressurized volume, with a mass of 24 tons, and can hold four times the standard atmospheric pressure. Moreover, the Whipple shield configuration is identical to the heavily protected sections of the ISS. The service module has a traditional cylindrical design and its role is to provide all the necessary utilities. Furthermore, the paper explains the assembly and welding method required to convert Orb2 into the fully assembled space station. I. Nomenclature LEO = low Earth orbit ISS = International Space Station PAS = payload adapter system MMOD = micrometeoroids and orbital debris FEA = finite element analysis g = gravitational force, 9:81m/s2 EBW = electron beam welding BEAM = Bigelow Expandable Activity Module ∗Staff Research Engineer, Portland, OR, 97201 USA, Member AIAA. -
The Annual Compendium of Commercial Space Transportation: 2017
Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents About the FAA Office of Commercial Space Transportation The Federal Aviation Administration’s Office of Commercial Space Transportation (FAA AST) licenses and regulates U.S. commercial space launch and reentry activity, as well as the operation of non-federal launch and reentry sites, as authorized by Executive Order 12465 and Title 51 United States Code, Subtitle V, Chapter 509 (formerly the Commercial Space Launch Act). FAA AST’s mission is to ensure public health and safety and the safety of property while protecting the national security and foreign policy interests of the United States during commercial launch and reentry operations. In addition, FAA AST is directed to encourage, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA AST’s website: http://www.faa.gov/go/ast Cover art: Phil Smith, The Tauri Group (2017) Publication produced for FAA AST by The Tauri Group under contract. NOTICE Use of trade names or names of manufacturers in this document does not constitute an official endorsement of such products or manufacturers, either expressed or implied, by the Federal Aviation Administration. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY .