Developing Technologies for Biological Experiments in Deep Space †
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Report of the Commission on the Scientific Case for Human Space Exploration
1 ROYAL ASTRONOMICAL SOCIETY Burlington House, Piccadilly London W1J 0BQ, UK T: 020 7734 4582/ 3307 F: 020 7494 0166 [email protected] www.ras.org.uk Registered Charity 226545 Report of the Commission on the Scientific Case for Human Space Exploration Professor Frank Close, OBE Dr John Dudeney, OBE Professor Ken Pounds, CBE FRS 2 Contents (A) Executive Summary 3 (B) The Formation and Membership of the Commission 6 (C) The Terms of Reference 7 (D) Summary of the activities/meetings of the Commission 8 (E) The need for a wider context 8 (E1) The Wider Science Context (E2) Public inspiration, outreach and educational Context (E3) The Commercial/Industrial context (E4) The Political and International context. (F) Planetary Science on the Moon & Mars 13 (G) Astronomy from the Moon 15 (H) Human or Robotic Explorers 15 (I) Costs and Funding issues 19 (J) The Technological Challenge 20 (J1) Launcher Capabilities (J2) Radiation (K) Summary 23 (L) Acknowledgements 23 (M) Appendices: Appendix 1 Expert witnesses consulted & contributions received 24 Appendix 2 Poll of UK Astronomers 25 Appendix 3 Poll of Public Attitudes 26 Appendix 4 Selected Web Sites 27 3 (A) Executive Summary 1. Scientific missions to the Moon and Mars will address questions of profound interest to the human race. These include: the origins and history of the solar system; whether life is unique to Earth; and how life on Earth began. If our close neighbour, Mars, is found to be devoid of life, important lessons may be learned regarding the future of our own planet. 2. While the exploration of the Moon and Mars can and is being addressed by unmanned missions we have concluded that the capabilities of robotic spacecraft will fall well short of those of human explorers for the foreseeable future. -
Orbital Debris Quarterly News 22-1
National Aeronautics and Space Administration Orbital Debris Quarterly News Volume 22, Issue 1 February 2018 Inside... Two Anomalous Events in GEO Summer 2017 was marred by two apparently platform. Spacecraft dry mass is estimated to be on Space Debris Sensor anomalous events in the geosynchronous orbit the order of 2000 kg. On-board stored energy sources Launches Aboard (GEO) belt. Both incidents have been observed by include fuel and pressurized components, as well as the commercial space situation awareness providers, but as battery subsystem. SpaceX-13 2 of 26 December 2017 no debris from either event have The Indonesian GEO communications spacecraft entered the public catalog. TELKOM-1 (1999-042A, SSN catalog number 25880) SEM Analysis The GEO communications spacecraft AMC-9 experienced an energetic event on or about 25 August Results of (International Designator 2003-024A, U.S. Strategic 2017, after over 18.1 years on-orbit—3 years past Returned ISS Command [USSTRATCOM] Space Surveillance its nominal operational lifetime. An examination of Network [SSN] catalog number 27820), formerly known the Two Line Element data indicates an observable PMA-2 Cover 4 as GE-12, experienced an energetic event estimated to change in spacecraft orbit between 26 and 29 August. have occurred at approximately 07:10 GMT on 17 June At the beginning of this time interval, approximately CubeSat Study 2017, after approximately 14 years on-orbit. Fig. 1 Project Review 6 depicts the orbital evolution of the spacecraft in 2017. continued on page 2 SES, the spacecraft owner- operator, described this AMC‐9 (SSN 27820, 2003‐024A) 360 36300 Space Debris Sensor event as a “serious anomaly.” Installation 8 Following this event, the 36200 spacecraft began a westward 300 Monthly Object Type drift in the GEO belt. -
The Cubesat Mission to Study Solar Particles (Cusp) Walt Downing IEEE Life Senior Member Aerospace and Electronic Systems Society President (2020-2021)
The CubeSat Mission to Study Solar Particles (CuSP) Walt Downing IEEE Life Senior Member Aerospace and Electronic Systems Society President (2020-2021) Acknowledgements – National Aeronautics and Space Administration (NASA) and CuSP Principal Investigator, Dr. Mihir Desai, Southwest Research Institute (SwRI) Feature Articles in SYSTEMS Magazine Three-part special series on Artemis I CubeSats - April 2019 (CuSP, IceCube, ArgoMoon, EQUULEUS/OMOTENASHI, & DSN) ▸ - September 2019 (CisLunar Explorers, OMOTENASHI & Iris Transponder) - March 2020 (BioSentinnel, Near-Earth Asteroid Scout, EQUULEUS, Lunar Flashlight, Lunar Polar Hydrogen Mapper, & Δ-Differential One-Way Range) Available in the AESS Resource Center https://resourcecenter.aess.ieee.org/ ▸Free for AESS members ▸ What are CubeSats? A class of small research spacecraft Built to standard dimensions (Units or “U”) ▸ - 1U = 10 cm x 10 cm x 11 cm (Roughly “cube-shaped”) ▸ - Modular: 1U, 2U, 3U, 6U or 12U in size - Weigh less than 1.33 kg per U NASA's CubeSats are dispensed from a deployer such as a Poly-Picosatellite Orbital Deployer (P-POD) ▸NASA’s CubeSat Launch initiative (CSLI) provides opportunities for small satellite payloads to fly on rockets ▸planned for upcoming launches. These CubeSats are flown as secondary payloads on previously planned missions. https://www.nasa.gov/directorates/heo/home/CubeSats_initiative What is CuSP? NASA Science Mission Directorate sponsored Heliospheric Science Mission selected in June 2015 to be launched on Artemis I. ▸ https://www.nasa.gov/feature/goddard/2016/heliophys ics-cubesat-to-launch-on-nasa-s-sls Support space weather research by determining proton radiation levels during solar energetic particle events and identifying suprathermal properties that could help ▸ predict geomagnetic storms. -
Space Station Intergovernmental Agreement
AGREEMENT AMONG THE GOVERNMENT OF CANADA, GOVERNMENTS OF MEMBER STATES OF THE EUROPEAN SPACE AGENCY, THJ3 GOVERNMENT OF JAPAN, THE GOVERNMENT OF THE RUSSIAN FEDERATION, AND THE GOVERNMENT OF THE UNITED STATES OF AMERICA CONCERNING COOPERATION ON THE CIVIL INTERNATIONAL SPACE STATION , - Table of Contents Arkle 1 Object and Scope Art~le 2 International Rights and Obhgatlons Article 3 Detimtlons Artxle 4 Cooperatmg Agencies Article 5 Reglstratlon, lunsd~cl~on and Control Article 6 Ownershrp of Elements and Equipment Article 7 Management Artxle 8 De&&d Des1811and Development Artde 9 Utthzation Article 10 Operation Article I I crew Article I2 Transportation Article 13 Communlcatrons Article I4 Evolution Article I5 Fundmg Article 16 Cross-Waiver of Liability Article I7 Llabillty Convention Article 18 Customs and Immigmtlon Article 19 Exchange of Data and Goods Article 20 Treatment of Data and Goods in Transit Article 2 1 Intellectual Property tiicle 22 Crimmal Junsdic~on Artxle 23 Consultations Article 24 Space StatIon Cooperation Review Alticle 25 Entry into Force Arlicle 26 Opmti~e Effect as between Certain PartIes Artxle 27 Amendments Article 28 Withdrawal Annex Space Station Elements to be Provided by the Partners I - II I The Government of Canada (heremafter also “Canada”), The Governments of the Kingdom of Belgium, the Kmgdom of Denmark, the French Republic, the Federal Republic of Germany, the Italian Repubhc, the Kmgdom of the Netherlands, the Kingdom of Norway, the Kingdom of Spam, the Kingdom of Sweden, the Swiss Confederation, and -
Lunar Flashlight & NEA Scout
National Aeronautics and Space Administration Lunar Flashlight & NEA Scout A NanoSat Architecture for Deep Space Exploration Payam Banazadeh (JPL/Caltech) Andreas Frick (JPL/Caltech) EM-1 Secondary Payload Selection • 19 NASA center-led concepts were evaluated and 3 were down-selected for further refinement by AES toward a Mission Concept Review (MCR) planned for August 2014 • Primary selection criteria: - Relevance to Space Exploration Strategic Knowledge Gaps (SKGs) - Life cycle cost - Synergistic use of previously demonstrated technologies - Optimal use of available civil servant workforce Payload Strategic Knowledge Gaps Mission Concept NASA Centers Addressed BioSentinel Human health/performance in high- Study radiation-induced DNA ARC/JSC radiation space environments damage of live organisms in cis- • Fundamental effects on biological systems lunar space; correlate with of ionizing radiation in space environments measurements on ISS and Earth Lunar Flashlight Lunar resource potential Locate ice deposits in the Moon’s JPL/MSFC/MHS • Quantity and distribution of water and other permanently shadowed craters volatiles in lunar cold traps Near Earth Asteroid (NEA) NEA Characterization Slow flyby/rendezvous and Scout • NEA size, rotation state (rate/pole position) characterize one NEA in a way MSFC/JPL How to work on and interact with NEA that is relevant to human surface exploration • NEA surface mechanical properties 2 EM-1: Near Earth Asteroid (NEA) Scout concept WHY NEA Scout? – Characterize a NEA with an imager to address key Strategic -
Selection of the Insight Landing Site M. Golombek1, D. Kipp1, N
Manuscript Click here to download Manuscript InSight Landing Site Paper v9 Rev.docx Click here to view linked References Selection of the InSight Landing Site M. Golombek1, D. Kipp1, N. Warner1,2, I. J. Daubar1, R. Fergason3, R. Kirk3, R. Beyer4, A. Huertas1, S. Piqueux1, N. E. Putzig5, B. A. Campbell6, G. A. Morgan6, C. Charalambous7, W. T. Pike7, K. Gwinner8, F. Calef1, D. Kass1, M. Mischna1, J. Ashley1, C. Bloom1,9, N. Wigton1,10, T. Hare3, C. Schwartz1, H. Gengl1, L. Redmond1,11, M. Trautman1,12, J. Sweeney2, C. Grima11, I. B. Smith5, E. Sklyanskiy1, M. Lisano1, J. Benardino1, S. Smrekar1, P. Lognonné13, W. B. Banerdt1 1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109 2State University of New York at Geneseo, Department of Geological Sciences, 1 College Circle, Geneseo, NY 14454 3Astrogeology Science Center, U.S. Geological Survey, 2255 N. Gemini Dr., Flagstaff, AZ 86001 4Sagan Center at the SETI Institute and NASA Ames Research Center, Moffett Field, CA 94035 5Southwest Research Institute, Boulder, CO 80302; Now at Planetary Science Institute, Lakewood, CO 80401 6Smithsonian Institution, NASM CEPS, 6th at Independence SW, Washington, DC, 20560 7Department of Electrical and Electronic Engineering, Imperial College, South Kensington Campus, London 8German Aerospace Center (DLR), Institute of Planetary Research, 12489 Berlin, Germany 9Occidental College, Los Angeles, CA; Now at Central Washington University, Ellensburg, WA 98926 10Department of Earth and Planetary Sciences, University of Tennessee, Knoxville, TN 37996 11Institute for Geophysics, University of Texas, Austin, TX 78712 12MS GIS Program, University of Redlands, 1200 E. Colton Ave., Redlands, CA 92373-0999 13Institut Physique du Globe de Paris, Paris Cité, Université Paris Sorbonne, France Diderot Submitted to Space Science Reviews, Special InSight Issue v. -
Global Ionosphere-Thermosphere-Mesosphere (ITM) Mapping Across Temporal and Spatial Scales a White Paper for the NRC Decadal
Global Ionosphere-Thermosphere-Mesosphere (ITM) Mapping Across Temporal and Spatial Scales A White Paper for the NRC Decadal Survey of Solar and Space Physics Andrew Stephan, Scott Budzien, Ken Dymond, and Damien Chua NRL Space Science Division Overview In order to fulfill the pressing need for accurate near-Earth space weather forecasts, it is essential that future measurements include both temporal and spatial aspects of the evolution of the ionosphere and thermosphere. A combination of high altitude global images and low Earth orbit altitude profiles from simple, in-the-medium sensors is an optimal scenario for creating continuous, routine space weather maps for both scientific and operational interests. The method presented here adapts the vast knowledge gained using ultraviolet airglow into a suggestion for a next-generation, near-Earth space weather mapping network. Why the Ionosphere, Thermosphere, and Mesosphere? The ionosphere-thermosphere-mesosphere (ITM) region of the terrestrial atmosphere is a complex and dynamic environment influenced by solar radiation, energy transfer, winds, waves, tides, electric and magnetic fields, and plasma processes. Recent measurements showing how coupling to other regions also influences dynamics in the ITM [e.g. Immel et al., 2006; Luhr, et al, 2007; Hagan et al., 2007] has exposed the need for a full, three- dimensional characterization of this region. Yet the true level of complexity in the ITM system remains undiscovered primarily because the fundamental components of this region are undersampled on the temporal and spatial scales that are necessary to expose these details. The solar and space physics research community has been driven over the past decade toward answering scientific questions that have a high level of practical application and relevance. -
Bolden Testimony
HOLD FOR RELEASE UNTIL PRESENTED BY WITNESS November 17, 2011 Statement of The Honorable Charles F. Bolden, Jr. Administrator National Aeronautics and Space Administration before the Subcommittee on Science and Space Committee on Commerce, Science and Transportation U. S. Senate Mr. Chairman and Members of the Subcommittee, thank you for the opportunity to appear before you today to discuss the outlook for NASA’s human space flight program. This has been a remarkable year, as we have completed assembling and outfitting of the U.S. On-orbit Segment (USOS) of the International Space Station (ISS), allowing us to focus on full utilization of the Station’s research capabilities; taken key steps in moving forward into the future of exploration beyond Low-Earth Orbit (LEO); celebrated the 50 th anniversary of human spaceflight; and witnessed the successful conclusion of the historic Space Shuttle Program. We are also pleased with the progress our industry partners have made in developing an American capability to transport cargo and eventually astronauts to the ISS, and end the outsourcing of this work to foreign governments. More importantly, this will add a critical level of redundancy for transporting cargo and crew to the ISS. A robust transportation architecture is important to ensuring full utilization of this amazing research facility. Enabling commercial crew and cargo transportation systems in LEO allows NASA to focus on developing its own systems for sending astronauts on missions of exploration beyond LEO. This split between commercial and Government systems allows for a cost effective approach to promote a broad base for human exploration by the United States. -
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. -
NASA's Ames Research Center
NASA’s Ames Research Center NASA’s center in Silicon Valley Ames Research Center, one of 10 NASA fi eld Ames provides NASA with advancements in: centers, is located in California’s Silicon Valley. For more than 70 years, Ames has been a leader in Entry systems: Safely delivering spacecraft to conducting world-class research and development. Earth and other celestial bodies. Location: California’s Silicon Valley, 40 miles Supercomputing: Enabling NASA’s advanced south of San Francisco; 12 miles north of San modeling and simulation. Jose, between Mountain View and Sunnyvale Next generation air transportation: Transforming Jobs: Approximately 2,500 on-site employees and the way we fl y. contractors Airborne science: Examining our own world and Economic impact: $1.3B annually for the U.S.; beyond from the sky. $932M for California and $877M for Bay Area, creating more than 8,400 jobs in the U.S. with Low-cost missions: Enabling high value science 5,900 in California (2010 Economic Benefi ts to low Earth orbit and the moon. Study). Biology and astrobiology: Understanding life on Established: Dec. 20, 1939 as part of the National Earth -- and in space. Advisory Committee for Aeronautics (NACA); became part of the National Aeronautics and Exoplanets: Finding worlds beyond our own. Space Administration (NASA) in 1958. Autonomy and robotics: Complementing Missions: Ames-related missions scheduled for humans in space. launch in 2013 include LADEE, PhoneSat, EDSN, EcAMSat, SporeSat and IRIS. Ames will launch Lunar science: Rediscovering our moon. several space biosciences payloads this year. The center is lead for the Mars Curiosity rover’s Human factors: Advancing human-technology Chemistry and Mineralogy (CheMin) instrument interaction for NASA missions. -
NASA's STEREO Mission
NASA’s STEREO Mission J.B. Gurman STEREO Project Scientist W.T. Thompson STEREO Chief Observer Solar Physics Laboratory, Helophysics Division NASA Goddard Space Flight Center 1 The STEREO Mission • Science and technology definition team report, 1997 December: • Understand the origin and consequences of coronal mass ejections (CMEs) • Two spacecraft in earth-leading and -lagging orbits near 1 AU (Solar Terrestrial Probe line) • “Beacon” mode for near-realtime warning of potentially geoeffective events 2 Level 1 Requirements • Understand the causes and mechanisms of CME initiation • Characterize the propagation of CMEs through the heliosphere • Discover the mechanisms and sites of energetic particle acceleration in the low corona and the interplanetary medium • Develop a 3D, time-dependent model of the magnetic topology, temperature, density, and velocity structure of the ambient solar wind 3 Implementation • Two nearly identical spacecraft launched by a single ELV • Bottom spacecraft in stack has adapter ring, some strengthening • Spacecraft built at Johns Hopkins University APL • Four science investigations 4 Scientific Instruments • S/WAVES - broad frequency response RF detection of Type II, III bursts • PLASTIC - solar wind plasma and suprathermal ion composition measurements • IMPACT - energetic electrons and ions, magnetic field • SECCHI - EUV, coronagraphs and heliospheric imagers (surface to 1.5 AU) 5 Instrument Hardware • PLASTIC IMPACT boom IMPACT boom SECCHI SCIP SECCHI HI S/WAVES 6 Orbit Design • Science team selected a separation -
Nustar Observatory Guide
NuSTAR Guest Observer Program NuSTAR Observatory Guide Version 3.2 (June 2016) NuSTAR Science Operations Center, California Institute of Technology, Pasadena, CA NASA Goddard Spaceflight Center, Greenbelt, MD nustar.caltech.edu heasarc.gsfc.nasa.gov/docs/nustar/index.html i Revision History Revision Date Editor Comments D1,2,3 2014-08-01 NuSTAR SOC Initial draft 1.0 2014-08-15 NuSTAR GOF Release for AO-1 Addition of more information about CZT 2.0 2014-10-30 NuSTAR SOC detectors in section 3. 3.0 2015-09-24 NuSTAR SOC Update to section 4 for release of AO-2 Update for NuSTARDAS v1.6.0 release 3.1 2016-05-10 NuSTAR SOC (nusplitsc, Section 5) 3.2 2016-06-15 NuSTAR SOC Adjustment to section 9 ii Table of Contents Revision History ......................................................................................................................................................... ii 1. INTRODUCTION ................................................................................................................................................... 1 1.1 NuSTAR Program Organization ..................................................................................................................................................................................... 1 2. The NuSTAR observatory .................................................................................................................................... 2 2.1 NuSTAR Performance ........................................................................................................................................................................................................