Small Spacecraft Technology State of the Art

Total Page:16

File Type:pdf, Size:1020Kb

Small Spacecraft Technology State of the Art NASA/TP–2015–216648/REV1 Small Spacecraft Technology State of the Art Mission Design Division Ames Research Center, Moffett Field, California December 2015 NASA STI Program . in Profile Since its founding, NASA has been dedicated • CONFERENCE PUBLICATION. to the advancement of aeronautics and space Collected papers from scientific and science. The NASA scientific and technical technical conferences, symposia, seminars, information (STI) program plays a key part or other meetings sponsored or in helping NASA maintain this important co-sponsored by NASA. role. • SPECIAL PUBLICATION. Scientific, The NASA STI Program operates under the technical, or historical information from auspices of the Agency Chief Information NASA programs, projects, and missions, Officer. It collects, organizes, provides for often concerned with subjects having archiving, and disseminates NASA’s STI. substantial public interest. The NASA STI Program provides access to the NASA Aeronautics and Space Database • TECHNICAL TRANSLATION. English- and its public interface, the NASA Technical language translations of foreign scientific Report Server, thus providing one of the and technical material pertinent to largest collection of aeronautical and space NASA’s mission. science STI in the world. Results are Specialized services also include creating published in both non-NASA channels and custom thesauri, building customized by NASA in the NASA STI Report Series, databases, and organizing and publishing which includes the following report types: research results. • TECHNICAL PUBLICATION. Reports of For more information about the NASA STI completed research or a major significant Program, see the following: phase of research that present the results of NASA programs and include extensive • Access the NASA STI program home page data or theoretical analysis. Includes compilations of significant scientific and at http://www.sti.nasa.gov technical data and information deemed to • E-mail your question via the Internet to be of continuing reference value. NASA [email protected] counterpart of peer-reviewed formal professional papers, but having less • Fax your question to the NASA STI Help stringent limitations on manuscript length Desk at 443-757-5803 and extent of graphic presentations. • TECHNICAL MEMORANDUM. • Phone the NASA STI Help Desk at Scientific and technical findings that are 443-757-5802 preliminary or of specialized interest, e.g., quick release reports, working papers, and • Write to: bibliographies that contain minimal NASA STI Help Desk annotation. Does not contain extensive NASA Center for AeroSpace Information analysis. 7115 Standard Drive Hanover, MD 21076–1320 • CONTRACTOR REPORT. Scientific and technical findings by NASA-sponsored contractors and grantees. NASA/TP–2015–216648/REV1 Small Spacecraft Technology State of the Art Mission Design Division Ames Research Center, Moffett Field, California National Aeronautics and Space Administration Ames Research Center Moffett Field, California 94035-1000 December 2015 The use of trademarks or names of manufacturers in this report is for accurate reporting and does not constitute an official endorsement, either expressed or implied, of such products or manufacturers by the National Aeronautics and Space Administration. Available from: NASA Center for AeroSpace Information National Technical Information Service 7115 Standard Drive 5301 Shawnee Road Hanover, MD 21076-1320 Alexandria, VA 22312 443-757-5802 703-605-6000 This report is also available in electronic form at Abstract This report provides an overview of the current state of the art of small spacecraft technology. It was first commissionedby NASA’s SmallSpaceraft Technology Program (SSTP) inmid-2013 in response to the rapid growth in interest in using small spacecraft for many types of missions in Earth orbit and beyond, and revised in mid-2015. For the sake of this assessment, small spacecraft are defined to be spacecraft with a mass less than 180 kg. This report provides a summary of the state of the art for each of the following small spacecraft technology domains: Complete Spacecraft, Power, Propulsion, Guidance Navigation and Control, Structures, Materials and Mechanisms, Thermal Control, Command and Data Handling, Communications, Integration, Launch and Deployment, Ground Data Systems and Operations, and Passive Deorbit Devices. Due to the high market penetration of cubesats, particular emphasis is placed on the state of the art of cubesat-related technology. 1 Disclaimer The document lists or describes many specific products and technologies as examples and references but their inclusion does not imply any endorsement by NASA. Failure to include any specific prod­ ucts or technologies that might be considered relevant under a particular topic was unintentional. Acknowledgements This report has been based largely on desktop research and published documents on small space­ craft technology, industry consultation and participation at conferences. Helpful suggestions and contributions were also received from numerous people at NASA Ames Research Center, and in par­ ticular the authors wish to acknowledge the reviewers James Bell, Josh Benton, Matt D’Ortenzio, Josh Forgione, Vanessa Kuroda, Dawn McIntosh, Marc Murbach, Matt Nehrenz, Hugo Sanchez, Matt Sorgenfrei, Sarah Thompson, Eddie Uribe and Bruce Yost. From NASA Glenn Research Center the authors would like to thank the reviewers Matt Deans, Fred Elliot, Josh Freeh, David Jacobson, William Marshall, Felix A. Miranda, Tim Smith and Brandon White. Finally, the authors would like to thank all of the compaines, universities and organizations who provided information for this report. 2 NASA Ames Research Center, Mission Design Division September, 2015 Division Chief: Chad Frost Project Manager: Elwood Agasid Editor: Rogan Shimmin Contributing Authors: Elwood Agasid, Roland Burton, Roberto Carlino, Gregory Defouw, Andres Dono Perez, Arif Göktuğ Karacalıoğlu, Benjamin Klamm, Abraham Rademacher, James Schalkwyck, Rogan Shimmin, Julia Tilles, Sasha Weston 3 Contents 1 Introduction 14 1.1 Objective .......................................... 14 1.2 Scope ............................................ 14 1.3 Assessment ......................................... 14 1.4 Overview .......................................... 15 2 Integrated Spacecraft Platforms 18 2.1 Introduction ......................................... 18 2.2 State of the Art ....................................... 18 2.3 On the Horizon ....................................... 22 2.4 Conclusion .......................................... 23 3 Power 25 3.1 Introduction ......................................... 25 3.2 State of the art ....................................... 25 3.2.1 Power Generation .................................. 25 3.2.2 Power Storage .................................... 28 3.2.3 Power Management and Distribution ....................... 32 3.3 On the horizon ....................................... 35 3.3.1 Power Generation .................................. 35 3.4 Conclusion .......................................... 38 4 Propulsion 40 4.1 Introduction ......................................... 40 4.2 State of the art ....................................... 41 4.2.1 Chemical Propulsion Systems ........................... 41 4.2.2 Electric Propulsion Systems ............................ 50 4.2.3 Propellant-less Systems .............................. 57 4.3 On the Horizon ....................................... 57 4.4 Conclusion .......................................... 60 5 Guidance, Navigation and Control 63 5.1 Introduction ......................................... 63 5.2 State of the art ....................................... 63 5.2.1 Integrated Units .................................. 63 5.2.2 Reaction Wheels .................................. 64 5.2.3 Magnetorquers ................................... 66 5.2.4 Thrusters ...................................... 66 5.2.5 Star Trackers .................................... 66 5.2.6 Magnetometers ................................... 66 5.2.7 Sun Sensors ..................................... 68 5.2.8 Earth Sensors .................................... 69 5.2.9 Gyros ........................................ 69 5.2.10 GPS ......................................... 71 5.2.11 Deep Space Navigation ............................... 71 5.3 On the Horizon ....................................... 72 5.4 Conclusion .......................................... 72 4 6 Structures, Materials and Mechanisms 74 6.1 Introduction . 74 6.2 State of the art . 74 6.2.1 Primary Structure . 75 6.2.2 Mechanisms . 76 6.3 On the Horizon . 78 6.4 Radiation Effects and Mitigation Strategies . 80 6.4.1 Shielding from the Space Environment . 80 6.4.2 Inherent Mass Shielding . 81 6.4.3 Ad Hoc Shielding . 82 6.5 Conclusion . 82 7 Thermal Control System 84 7.1 Introduction . 84 7.2 State of the Art . 84 7.2.1 Passive Systems . 84 7.2.2 Active Systems . 88 7.3 On the Horizon . 93 7.4 Conclusion . 95 8 Command and Data Handling 98 8.1 Introduction . 98 8.2 State of the art . 98 8.2.1 Form Factor . 98 8.2.2 On-Board Computing . 98 8.2.3 Memory and Electronic Components . 100 8.2.4 Bus Electrical Interfaces and I/O . 103 8.2.5 Electronic Power Supplies . 104 8.3 On the Horizon . 104 8.4 Radiation mitigation and tolerance schemes . 104 8.4.1 Radiation mitigation and tolerance schemes . 105 8.4.2 Component Selection . 105 8.4.3 Protection Circuits . 105 8.4.4 Memory Protection . 106 8.4.5 Communication Protection . 106 8.4.6 Parallel Processing
Recommended publications
  • Preface Patrick Besha, Editor Alexander Macdonald, Editor in The
    EARLY DRAFT - NASAWATCH.COM/SPACEREF.COM Preface Patrick Besha, Editor Alexander MacDonald, Editor In the next decade, NASA will seek to expand humanity’s presence in space beyond the International Space Station in low-Earth orbit to a new habitation platform orbiting the moon. By the late 2020’s, astronauts will live and work far deeper in space than ever before. The push to cis-lunar orbit is part of a stepping-stone approach to extend our reach to Mars and beyond. This decision to explore ever farther destinations is a familiar pattern in the history of American space exploration. Another major pattern with historical precedent is the transition from public sector exploration to private sector commercialization. After the government has developed and demonstrated a capability in space, whether it be space-based communications or remote sensing, the private sector has realized its market potential. As new companies establish a presence, the government withdraws from the market. In 2015, we are once again at a critical stage in the development of space. The most successful long-term human habitation in space, orbiting the Earth continuously since 1998, is the International Space Station. Currently at the apex of its capabilities and the pinnacle of state-of-the-art space systems, it was developed through the investments and labors of over a dozen nations and is regularly re-supplied by cargo delivery services. Its occupants include six astronauts and numerous other organisms from Earth’s ecosystems from bacteria to plants to rats. Research is conducted on the spacecraft from hundreds of organizations worldwide ranging from academic institutions to large industrial companies and from high-tech start-ups to high-school science classes.
    [Show full text]
  • Cape Canaveral Air Force Station Support to Commercial Space Launch
    The Space Congress® Proceedings 2019 (46th) Light the Fire Jun 4th, 3:30 PM Cape Canaveral Air Force Station Support to Commercial Space Launch Thomas Ste. Marie Vice Commander, 45th Space Wing Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Ste. Marie, Thomas, "Cape Canaveral Air Force Station Support to Commercial Space Launch" (2019). The Space Congress® Proceedings. 31. https://commons.erau.edu/space-congress-proceedings/proceedings-2019-46th/presentations/31 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Cape Canaveral Air Force Station Support to Commercial Space Launch Colonel Thomas Ste. Marie Vice Commander, 45th Space Wing CCAFS Launch Customers: 2013 Complex 41: ULA Atlas V (CST-100) Complex 40: SpaceX Falcon 9 Complex 37: ULA Delta IV; Delta IV Heavy Complex 46: Space Florida, Navy* Skid Strip: NGIS Pegasus Atlantic Ocean: Navy Trident II* Black text – current programs; Blue text – in work; * – sub-orbital CCAFS Launch Customers: 2013 Complex 39B: NASA SLS Complex 41: ULA Atlas V (CST-100) Complex 40: SpaceX Falcon 9 Complex 37: ULA Delta IV; Delta IV Heavy NASA Space Launch System Launch Complex 39B February 4, 2013 Complex 46: Space Florida, Navy* Skid Strip: NGIS Pegasus Atlantic Ocean: Navy Trident II* Black text – current programs;
    [Show full text]
  • A Middleware Framework for Application-Aware and User-Specific Energy Optimization in Smart Mobile Devices
    Pervasive and Mobile Computing 20 (2015) 47–63 Contents lists available at ScienceDirect Pervasive and Mobile Computing journal homepage: www.elsevier.com/locate/pmc A middleware framework for application-aware and user-specific energy optimization in smart mobile devices Sudeep Pasricha a,∗, Brad K. Donohoo b, Chris Ohlsen c a Colorado State University, Fort Collins, CO 80523, USA b U.S. Department of the Air Force, Roy, UT 84067, UT 84067, USA c Woodward, Inc., Fort Collins, CO 80525, USA article info a b s t r a c t Article history: Mobile battery-operated devices are becoming an essential instrument for business, com- Received 5 August 2014 munication, and social interaction. In addition to the demand for an acceptable level of per- Received in revised form 22 December 2014 formance and a comprehensive set of features, users often desire extended battery lifetime. Accepted 7 January 2015 In fact, limited battery lifetime is one of the biggest obstacles facing the current utility and Available online 14 January 2015 future growth of increasingly sophisticated ``smart'' mobile devices. This paper proposes a novel application-aware and user-interaction aware energy optimization middleware Keywords: framework (AURA) for pervasive mobile devices. AURA optimizes CPU and screen back- Energy optimization Smart mobile systems light energy consumption while maintaining a minimum acceptable level of performance. Pervasive computing The proposed framework employs a novel Bayesian application classifier and management Machine learning strategies based on Markov Decision Processes and Q-Learning to achieve energy savings. Middleware Real-world user evaluation studies on Google Android based HTC Dream and Google Nexus One smartphones running the AURA framework demonstrate promising results, with up to 29% energy savings compared to the baseline device manager, and up to 5×savings over prior work on CPU and backlight energy co-optimization.
    [Show full text]
  • Human Issues Related to Spacecraft Vibration During Ascent
    Human Issues related to Spacecraft Vibration during Ascent Consultant Report to the Constellation Program Standing Review Board Jonathan B. Clark M.D., M.P.H. Suite NA 425 One Baylor Plaza Baylor College of Medicine Houston TX 77030-3498 1731 Sunset Blvd Houston TX 77005 713 859 1381 281 989 8721 [email protected] [email protected] Opinions expressed herein are those of the author and do not reflect the views of the National Space Biomedical Research Institute (NSBRI), Baylor College of Medicine (BCM), the University of Texas Medical Branch (UTMB), or the National Aeronautics and Space Administration (NASA). Human Issues related to Spacecraft Vibration during Ascent Consultant Report to the Constellation Program Standing Review Board Jonathan B. Clark M.D., M.P.H. Opinions expressed herein are those of the author and do not reflect the views of the National Space Biomedical Research Institute (NSBRI), Baylor College of Medicine (BCM), the University of Texas Medical Branch (UTMB), or the National Aeronautics and Space Administration (NASA). Pogo in Liquid Fueled Rocket Motors The pogo phenomenon, or fuel pump inlet pressure fluctuation/ cavitation due to tuning feed line resonant frequencies was a major concern in the early space program. Pump tests showed that as inlet pressures were reduced toward cavitation, the pump started acting as an amplifier, causing large oscillations in the thrust chamber pressure. As the rocket engine thrust develops, liquid propellant is cyclically forced into the turbopump. This fluctuating fluid pressure is converted into an unintended and variable increase in engine thrust, with the net effect being longitudinal axis vibration that could result in spacecraft structural failure.
    [Show full text]
  • 2014 BT Compatibility List 20141030
    Item Brand Name Model 1 Acer Acer beTouch E210 2 Acer acer E400 3 Acer acer P400 4 Acer DX650 5 Acer E200 6 Acer Liquid E 7 Acer Liquid Mini (E310) 8 Acer M900 9 Acer S110 10 Acer Smart handheld 11 Acer Smart handheld 12 Acer Smart handheld E100 13 Acer Smart handheld E101 14 Adec & Partner AG AG vegas 15 Alcatel Alcatel OneTouch Fierce 2 16 Alcatel MISS SIXTY MSX10 17 Alcatel OT-800/ OT-800A 18 Alcatel OT-802/ OT-802A 19 Alcatel OT-806/ OT-806A/ OT-806D/ OT-807/ OT-807A/ OT-807D 20 Alcatel OT-808/ OT-808A 21 Alcatel OT-880/ OT-880A 22 Alcatel OT-980/ OT-980A 23 Altek Altek A14 24 Amazon Amazon Fire Phone 25 Amgoo Telecom Co LTD AM83 26 Apple Apple iPhone 4S 27 Apple Apple iPhone 5 28 Apple Apple iPhone 6 29 Apple Apple iPhone 6 Plus 30 Apple iPhone 2G 31 Apple iPhone 3G 32 Apple iPhone 3Gs 33 Apple iPhone 4 34 Apple iPhone 5C 35 Apple iPHone 5S 36 Aramasmobile.com ZX021 37 Ascom Sweden AB 3749 38 Asustek 1000846 39 Asustek A10 40 Asustek G60 41 Asustek Galaxy3_L and Galaxy3_S 42 Asustek Garmin-ASUS M10E 43 Asustek P320 44 Asustek P565c 45 BlackBerry BlackBerry Passport 46 BlackBerry BlackBerry Q10 47 Broadcom Corporation BTL-A 48 Casio Hitachi C721 49 Cellnet 7 Inc. DG-805 Cellon Communications 50 C2052, Technology(Shenzhen) Co., Ltd. Cellon Communications 51 C2053, Technology(Shenzhen) Co., Ltd. Cellon Communications 52 C3031 Technology(Shenzhen) Co., Ltd. Cellon Communications 53 C5030, Technology(Shenzhen) Co., Ltd.
    [Show full text]
  • Pocketqube Standard Issue 1 7Th of June, 2018
    The PocketQube Standard Issue 1 7th of June, 2018 The PocketQube Standard June 7, 2018 Contributors: Organization Name Authors Reviewers TU Delft S. Radu S. Radu TU Delft M.S. Uludag M.S. Uludag TU Delft S. Speretta S. Speretta TU Delft J. Bouwmeester J. Bouwmeester TU Delft - A. Menicucci TU Delft - A. Cervone Alba Orbital A. Dunn A. Dunn Alba Orbital T. Walkinshaw T. Walkinshaw Gauss Srl P.L. Kaled Da Cas P.L. Kaled Da Cas Gauss Srl C. Cappelletti C. Cappelletti Gauss Srl - F. Graziani Important Note(s): The latest version of the PocketQube Standard shall be the official version. 2 The PocketQube Standard June 7, 2018 Contents 1. Introduction ............................................................................................................................................................... 4 1.1 Purpose .............................................................................................................................................................. 4 2. PocketQube Specification ......................................................................................................................................... 4 1.2 General requirements ....................................................................................................................................... 5 2.2 Mechanical Requirements ................................................................................................................................. 5 2.2.1 Exterior dimensions ..................................................................................................................................
    [Show full text]
  • Cubesat Data Analysis Revision
    371-XXXXX Revision - CubeSat Data Analysis Revision - November 2015 Prepared by: GSFC/Code 371 National Aeronautics and Goddard Space Flight Center Space Administration Greenbelt, Maryland 20771 371-XXXXX Revision - Signature Page Prepared by: ___________________ _____ Mark Kaminskiy Date Reliability Engineer ARES Corporation Accepted by: _______________________ _____ Nasir Kashem Date Reliability Lead NASA/GSFC Code 371 1 371-XXXXX Revision - DOCUMENT CHANGE RECORD REV DATE DESCRIPTION OF CHANGE LEVEL APPROVED - Baseline Release 2 371-XXXXX Revision - Table of Contents 1 Introduction 4 2 Statement of Work 5 3 Database 5 4 Distributions by Satellite Classes, Users, Mass, and Volume 7 4.1 Distribution by satellite classes 7 4.2 Distribution by satellite users 8 4.3 CubeSat Distribution by mass 8 4.4 CubeSat Distribution by volume 8 5 Annual Number of CubeSats Launched 9 6 Reliability Data Analysis 10 6.1 Introducing “Time to Event” variable 10 6.2 Probability of a Successful Launch 10 6.3 Estimation of Probability of Mission Success after Successful Launch. Kaplan-Meier Nonparametric Estimate and Weibull Distribution. 10 6.3.1 Kaplan-Meier Estimate 10 6.3.2 Weibull Distribution Estimation 11 6.4 Estimation of Probability of mission success after successful launch as a function of time and satellite mass using Weibull Regression 13 6.4.1 Weibull Regression 13 6.4.2 Data used for estimation of the model parameters 13 6.4.3 Comparison of the Kaplan-Meier estimates of the Reliability function and the estimates based on the Weibull regression 16 7 Conclusion 17 8 Acknowledgement 18 9 References 18 10 Appendix 19 Table of Figures Figure 4-1 CubeSats distribution by mass ....................................................................................................
    [Show full text]
  • Ground-Based Demonstration of Cubesat Robotic Assembly
    Ground-based Demonstration of CubeSat Robotic Assembly CubeSat Development Workshop 2020 Ezinne Uzo-Okoro, Mary Dahl, Emily Kiley, Christian Haughwout, Kerri Cahoy 1 Motivation: In-Space Small Satellite Assembly Why not build in space? GEO MEO LEO The standardization of electromechanical CubeSat components for compatibility with CubeSat robotic assembly is a key gap 2 Goal: On-Demand On-Orbit Assembled CubeSats LEO Mission Key Phases ➢ Ground Phase: Functional electro/mechanical prototype ➢ ISS Phase: Development and launch of ISS flight unit locker, with CubeSat propulsion option ➢ Free-Flyer Phase: Development of agile free-flyer “locker” satellite with robotic arms to assemble and deploy rapid response CubeSats GEO ➢ Constellation Phase: Development of strategic constellation of agile free-flyer “locker” satellites with robotic Internal View of ‘Locker’ Showing Robotic Assembly arms to autonomously assemble and deploy CubeSats IR Sensors VIS Sensors RF Sensors Propulsion Mission Overview Mission Significance • Orbit-agnostic lockers deploy on-demand robot-assembled CubeSats Provides many CubeSat configurations responsive to • ‘Locker’ is mini-fridge-sized spacecraft with propulsion rapidly evolving space needs capability ✓ Flexible: Selectable sensors and propulsion • Holds robotic arms, sensor, and propulsion modules for ✓ Resilient: Dexterous robot arms for CubeSat assembly 1-3U CubeSats without humans-in-the-loop on Earth and on-orbit Build • Improve response: >30 days to ~hours custom-configured CubeSats on Earth or in space saving
    [Show full text]
  • Rideshare and the Orbital Maneuvering Vehicle: the Key to Low-Cost Lagrange-Point Missions
    SSC15-II-5 Rideshare and the Orbital Maneuvering Vehicle: the Key to Low-cost Lagrange-point Missions Chris Pearson, Marissa Stender, Christopher Loghry, Joe Maly, Valentin Ivanitski Moog Integrated Systems 1113 Washington Avenue, Suite 300, Golden, CO, 80401; 303 216 9777, extension 204 [email protected] Mina Cappuccio, Darin Foreman, Ken Galal, David Mauro NASA Ames Research Center PO Box 1000, M/S 213-4, Moffett Field, CA 94035-1000; 650 604 1313 [email protected] Keats Wilkie, Paul Speth, Trevor Jackson, Will Scott NASA Langley Research Center 4 West Taylor Street, Mail Stop 230, Hampton, VA, 23681; 757 864 420 [email protected] ABSTRACT Rideshare is a well proven approach, in both LEO and GEO, enabling low-cost space access through splitting of launch charges between multiple passengers. Demand exists from users to operate payloads at Lagrange points, but a lack of regular rides results in a deficiency in rideshare opportunities. As a result, such mission architectures currently rely on a costly dedicated launch. NASA and Moog have jointly studied the technical feasibility, risk and cost of using an Orbital Maneuvering Vehicle (OMV) to offer Lagrange point rideshare opportunities. This OMV would be launched as a secondary passenger on a commercial rocket into Geostationary Transfer Orbit (GTO) and utilize the Moog ESPA secondary launch adapter. The OMV is effectively a free flying spacecraft comprising a full suite of avionics and a propulsion system capable of performing GTO to Lagrange point transfer via a weak stability boundary orbit. In addition to traditional OMV ’tug’ functionality, scenarios using the OMV to host payloads for operation at the Lagrange points have also been analyzed.
    [Show full text]
  • Astrobiology in Low Earth Orbit
    The O/OREOS Mission – Astrobiology in Low Earth Orbit P. Ehrenfreund1, A.J. Ricco2, D. Squires2, C. Kitts3, E. Agasid2, N. Bramall2, K. Bryson4, J. Chittenden2, C. Conley5, A. Cook2, R. Mancinelli4, A. Mattioda2, W. Nicholson6, R. Quinn7, O. Santos2, G. Tahu5, M. Voytek5, C. Beasley2, L. Bica3, M. Diaz-Aguado2, C. Friedericks2, M. Henschke2, J.W. Hines2, D. Landis8, E. Luzzi2, D. Ly2, N. Mai2, G. Minelli2, M. McIntyre2, M. Neumann3, M. Parra2, M. Piccini2, R. Rasay3, R. Ricks2, A. Schooley2, E. Stackpole2, L. Timucin2, B. Yost2, A. Young3 1Space Policy Institute, Washington, DC, USA [email protected], 2NASA Ames Research Center, Moffett Field, CA, USA, 3Robotic Systems Laboratory, Santa Clara University, Santa Clara, CA, USA, 4Bay Area Environmental Research Institute, Sonoma, CA, USA, 5NASA Headquarters, Washington DC, USA, 6University of Florida, Gainesville, FL, USA, 7SETI Institute, Mountain View, CA, USA, 8Draper Laboratory, Cambridge, MA, USA Abstract. The O/OREOS (Organism/Organic Exposure to Orbital Stresses) nanosatellite is the first science demonstration spacecraft and flight mission of the NASA Astrobiology Small- Payloads Program (ASP). O/OREOS was launched successfully on November 19, 2010, to a high-inclination (72°), 650-km Earth orbit aboard a US Air Force Minotaur IV rocket from Kodiak, Alaska. O/OREOS consists of 3 conjoined cubesat (each 1000 cm3) modules: (i) a control bus, (ii) the Space Environment Survivability of Living Organisms (SESLO) experiment, and (iii) the Space Environment Viability of Organics (SEVO) experiment. Among the innovative aspects of the O/OREOS mission are a real-time analysis of the photostability of organics and biomarkers and the collection of data on the survival and metabolic activity for micro-organisms at 3 times during the 6-month mission.
    [Show full text]
  • The O/OREOS Mission—Astrobiology in Low Earth Orbit
    Acta Astronautica 93 (2014) 501–508 Contents lists available at ScienceDirect Acta Astronautica journal homepage: www.elsevier.com/locate/actaastro The O/OREOS mission—Astrobiology in low Earth orbit P. Ehrenfreund a,n, A.J. Ricco b, D. Squires b, C. Kitts c, E. Agasid b, N. Bramall b, K. Bryson d, J. Chittenden b, C. Conley e, A. Cook b, R. Mancinelli d, A. Mattioda b, W. Nicholson f, R. Quinn g, O. Santos b,G.Tahue,M.Voyteke, C. Beasley b,L.Bicac, M. Diaz-Aguado b, C. Friedericks b,M.Henschkeb,D.Landish, E. Luzzi b,D.Lyb, N. Mai b, G. Minelli b,M.McIntyreb,M.Neumannc, M. Parra b, M. Piccini b, R. Rasay c,R.Ricksb, A. Schooley b, E. Stackpole b, L. Timucin b,B.Yostb, A. Young c a Space Policy Institute, Washington DC, USA b NASA Ames Research Center, Moffett Field, CA, USA c Robotic Systems Laboratory, Santa Clara University, Santa Clara, CA, USA d Bay Area Environmental Research Institute, Sonoma, CA, USA e NASA Headquarters, Washington DC, USA f University of Florida, Gainesville, FL, USA g SETI Institute, Mountain View, CA, USA h Draper Laboratory, Cambridge, MA, USA article info abstract Article history: The O/OREOS (Organism/Organic Exposure to Orbital Stresses) nanosatellite is the first Received 19 December 2011 science demonstration spacecraft and flight mission of the NASA Astrobiology Small- Received in revised form Payloads Program (ASP). O/OREOS was launched successfully on November 19, 2010, to 22 June 2012 a high-inclination (721), 650-km Earth orbit aboard a US Air Force Minotaur IV rocket Accepted 18 September 2012 from Kodiak, Alaska.
    [Show full text]
  • The Annual Compendium of Commercial Space Transportation: 2012
    Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2012 February 2013 About FAA 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 (2013) 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. • i • Federal Aviation Administration’s Office of Commercial Space Transportation Dear Colleague, 2012 was a very active year for the entire commercial space industry. In addition to all of the dramatic space transportation events, including the first-ever commercial mission flown to and from the International Space Station, the year was also a very busy one from the government’s perspective. It is clear that the level and pace of activity is beginning to increase significantly.
    [Show full text]