An Evaluation of the Exposure in Nadir Observation of the JEM-EUSO Mission

Total Page:16

File Type:pdf, Size:1020Kb

An Evaluation of the Exposure in Nadir Observation of the JEM-EUSO Mission An evaluation of the exposure in nadir observation of the JEM-EUSO mission J.H. Adams Jr.md, S. Ahmadba, J.-N. Albertba, D. Allardbb, M. Ambrosiodf , L. Anchordoquime, A. Anzalonedh, Y. Araieu, C. Aramodf , K. Asanoes, M. Avekf , P. Barrillonba, T. Batschhc, J. Bayercd, T. Belenguerkb, R. Bellottidb, A.A. Berlindmg, M. Bertainadl,dk,1, P.L. Biermanncb, S. Biktemerovaia, C. Blaksleybb, J. B l¸eckihe, S. Blin-Bondilba, J. Bl¨umercb, P. Bobikja, M. Bogomilovaa, M. Bonamentemd, M.S. Briggsmd, S. Brizke, A. Brunoda, F. Cafagnada, D. Campanadf , J-N. Capdeviellebb, R. Carusodc, M. Casolinoev,di,dj, C. Cassardodl,dk, G. Castellinidd, O. Catalanodh, A. Cellinodm,dk, M. Chikawaed, M.J. Christlmf , V. Connaughtonmd, J.F. Cort´eske, H.J. Crawfordma, R. Cremoninidl, S. Csornamg, J.C. D’Olivoga, S. Dagoret-Campagneba, A.J. de Castroke, C. De Donatodi,dj, C. de la Tailleba, L. del Peralkd, A. Dell’Orodm,dk M.P. De Pascaledi,dj, M. Di Martinodm,dk, G. Distratiscd, M. Dupieuxbc, A. Ebersoldtcb, T. Ebisuzakiev, R. Engelcb, S. Falkcb, K. Fangmb, F. Fenucd, I. Fern´andez-G´omezke, S. Ferraresedl,dk, A. Franceschide, J. Fujimotoeu, P. Galeottidl,dk, G. Garipovic, J. Gearymd, U.G. Giaccaridf , G. Giraudodk, M. Goncharia, C. Gonz´alez Alvaradokb, P. Gorodetzkybb, F. Guarinodf,dg, A. Guzm´ancd, Y. Hachisuev, B. Harlovib, A. Haungscb, J. Hern´andez Carreterokd, K. Higashideeq,ev, T. Iguchi ei, H. Ikedaeo, N. Inoueeq, S. Inoueet, A. Insoliadc, F. Isgr`odf,dg, Y. Itowen, E. Jovenkg, E.G. Juddma, A. Jungfc, F. Kajinoei, T. Kajinoel, I. Kanekoev, Y. Karadzhovaa, J. Karczmarczykhc, K. Katahiraev, K. Kawaiev, Y. Kawasakiev, B. Keilhauercb, B.A. Khrenovic, Jeong-Sook Kimfb, Soon-Wook Kimfb, Sug-Whan Kimfd, M. Kleifgescb, P.A. Klimovic, S.H. Kofa, D. Kolevaa, I. Kreykenbohmca, K. Kudelaja, Y. Kuriharaeu, E. Kuznetsovmd, G. La Rosadh, J. Leefc, J. Licandrokg, H. Limfc, F. L´opezke, M.C. Maccaronedh, K. Mannheimce, L. Marcellidi,dj, A. Marinide, G. Martin-Chassardba, O. Martinezgc, G. Masciantoniodi,dj, K. Maseea, R. Matevaa, A. Maurissenla, G. Medina-Tancoga, T. Mernikcd, H. Miyamotoev, Y. Miyazakiec, Y. Mizumotoel, G. Modestinode, D. Monnier-Ragaigneba, J.A. Morales de los R´ıoskd, B. Motbc, T. Murakamief , M. Naganoec, M. Nagataeh, S. Nagatakiek, T. Nakamuraej, J.W. Namfc, S. Namfc, K. Namfc, T. Napolitanode, D. Naumovia, A. Neronovlb, et ev ev mb he arXiv:1305.2478v1 [astro-ph.HE] 11 May 2013 K. Nomoto , T. Ogawa , H. Ohmori , A.V. Olinto , P. Orlea´nski , G. Osteriadf , N. Pachecokc, M.I. Panasyukic, E. Parizotbb, I.H. Parkfc, B. Pastircakja, T. Patzakbb, T. Paulme, C. Pennypackerma, T. Peterlc, P. Picozzadi,dj,ev, A. Pollinila, H. Prietokd,ka, P. Reardonmd, M. Reinakb, M. Reyeskg, M. Riccide, I. Rodr´ıguezke, M.D. Rodr´ıguez Fr´ıaskd, F. Rongade, H. Rothkaehlhe, G. Roudilbc, I. Rusinovaa, M. Rybczy´nskiha, M.D. Sabaukb, G. S´aez Canokd, A. Saitoej , N. Sakakicb, M. Sakataei, H. Salazargc, S. S´anchezke, A. Santangelocd, L. Santiago Cr´uzga, M. Sanz Palominokb, O. Saprykinib, F. Sarazinmc, H. Satoei, M. Satoer, T. Schanzcd, H. Schielercb, V. Scottidf,dg, M. Scuderidc, A. Segretodh, S. Selmanebb, D. Semikozbb, Preprint submitted to Elsevier May 14, 2013 M. Serrakg, S. Sharakinic, T. Shibataep, H.M. Shimizuem, K. Shinozakiev,1, T. Shirahamaeq, G. Siemieniec-Ozi¸eb lohb, H.H. Silva L´opezga, J. Sleddmf , K. S lomi´nskahe, A. Sobeymf , T. Sugiyamaem, D. Supanitskyga, M. Suzukieo, B. Szabelskahc, J. Szabelskihc, F. Tajimaee, N. Tajimaev, T. Tajimacc, Y. Takahashier, H. Takamieu, M. Takedaeg, Y. Takizawaev, C. Tenzercd, O. Tibollace, L. Tkachevia, T. Tomidaev, N. Toneev, F. Trillaudga, R. Tsenovaa, K. Tsunoev, T. Tymienieckahd, Y. Uchihorieb, O. Vaduvescukg, J.F. Vald´es-Galiciaga, P. Vallaniadm,dk, L. Valoredf , G. Vankovaaa, C. Vigoritodl,dk, L. Villase˜norgb, P. von Ballmoosbc, S. Wadaev, J. Watanabeel, S. Watanabeer, J. Watts Jr.md, M. Webercb, T.J. Weilermg, T. Wibighc, L. Wienckemc, M. Willeca, J. Wilmsca, Z. W lodarczykha, T. Yamamotoei, Y. Yamamotoei, J. Yangfc, H. Yanoeo, I.V. Yashinic, D. Yonetokuef , K. Yoshidaei, S. Yoshidaea, R. Youngmf , A. Zamoraga, A. Zuccaro Marchiev aa St. Kliment Ohridski University of Sofia, Bulgaria ba Laboratoire de l’Acc´el´erateur Lin´eaire, Univ Paris Sud-11, CNES/IN2P3, Orsay, France bb APC, Univ Paris Diderot, CNRS/IN2P3, CEA/Irfu, Obs de Paris, Sorbonne Paris Cit´e, France bc IRAP, Universit´ede Toulouse, CNRS, Toulouse, France ca ECAP, University of Erlangen-Nuremberg, Germany cb Karlsruhe Institute of Technology (KIT), Germany cc Ludwig Maximilian University, Munich, Germany cd Institute for Astronomy and Astrophysics, Kepler Center, University of T¨ubingen, Germany ce Institute for Theoretical Physics and Astrophysics, University of W¨urzburg, Germany da Istituto Nazionale di Fisica Nucleare - Sezione di Bari, Italy db Universita’degli Studi di Bari Aldo Moro and INFN - Sezione di Bari, Italy dc Dipartimento di Fisica e Astronomia - Universita’ di Catania, Italy dd Consiglio Nazionale delle Ricerche - Istituto Nazionale di Ottica Firenze, Italy de Istituto Nazionale di Fisica Nucleare - Laboratori Nazionali di Frascati, Italy df Istituto Nazionale di Fisica Nucleare - Sezione di Napoli, Italy dg Universita’ di Napoli Federico II - Dipartimento di Scienze Fisiche, Italy dh INAF - Istituto di Astrofisica Spaziale e Fisica Cosmica di Palermo, Italy di Istituto Nazionale di Fisica Nucleare - Sezione di Roma Tor Vergata, Italy dj Universita’ di Roma Tor Vergata - Dipartimento di Fisica, Roma, Italy dk Istituto Nazionale di Fisica Nucleare - Sezione di Torino, Italy dl Dipartimento di Fisica, Universita’ di Torino, Italy dm Osservatorio Astrofisico di Torino, Istituto Nazionale di Astrofisica, Italy ea Chiba University, Chiba, Japan eb National Institute of Radiological Sciences, Chiba, Japan ec Fukui University of Technology, Fukui, Japan ed Kinki University, Higashi-Osaka, Japan ee Hiroshima University, Hiroshima, Japan ef Kanazawa University, Kanazawa, Japan eg Institute for Cosmic Ray Research, University of Tokyo, Kashiwa, Japan eh Kobe University, Kobe, Japan ei Konan University, Kobe, Japan ej Kyoto University, Kyoto, Japan ek Yukawa Institute, Kyoto University, Kyoto, Japan el National Astronomical Observatory, Mitaka, Japan em Nagoya University, Nagoya, Japan en Solar-Terrestrial Environment Laboratory, Nagoya University, Nagoya, Japan eo Institute of Space and Astronautical Science/JAXA, Sagamihara, Japan ep Aoyama Gakuin University, Sagamihara, Japan eq Saitama University, Saitama, Japan 2 er Hokkaido University, Sapporo, Japan es Interactive Research Center of Science, Tokyo Institute of Technology, Tokyo, Japan et University of Tokyo, Tokyo, Japan eu High Energy Accelerator Research Organization (KEK), Tsukuba, Japan ev RIKEN Advanced Science Institute, Wako, Japan fa Korea Advanced Institute of Science and Technology (KAIST), Daejeon, Republic of Korea fb Korea Astronomy and Space Science Institute (KASI), Daejeon, Republic of Korea fc Ewha Womans University, Seoul, Republic of Korea fd Center for Galaxy Evolution Research, Yonsei University, Seoul, Republic of Korea ga Universidad Nacional Aut´onoma de M´exico (UNAM), Mexico gb Universidad Michoacana de San Nicolas de Hidalgo (UMSNH), Morelia, Mexico gc Benem´erita Universidad Aut´onoma de Puebla (BUAP), Mexico ha Jan Kochanowski University, Institute of Physics, Kielce, Poland hb Jagiellonian University, Astronomical Observatory, Krakow, Poland hc National Centre for Nuclear Research, Lodz, Poland hd Cardinal Stefan Wyszy´nski University in Warsaw, Poland he Space Research Centre of the Polish Academy of Sciences (CBK), Warsaw, Poland ia Joint Institute for Nuclear Research, Dubna, Russia ib Central Research Institute of Machine Building, TsNIIMash, Korolev, Russia ic Skobeltsyn Institute of Nuclear Physics, Lomonosov Moscow State University, Russia ja Institute of Experimental Physics, Kosice, Slovakia ka Consejo Superior de Investigaciones Cient´ıficas (CSIC), Madrid, Spain kb Instituto Nacional de T´ecnica Aeroespacial (INTA), Madrid, Spain kc Instituto de F´ısica Te´orica, Universidad Aut´onoma de Madrid, Spain kd Universidad de Alcal´a(UAH), Madrid, Spain ke Universidad Carlos III de Madrid, Spain kf Universidad de Santiago de Compostela, Spain kg Instituto de Astrof´ısico de Canarias (IAC), Tenerife, Spain la Swiss Center for Electronics and Microtechnology (CSEM), Neuchˆatel, Switzerland lb ISDC Data Centre for Astrophysics, Versoix, Switzerland lc Institute for Atmospheric and Climate Science, ETH Z¨urich, Switzerland ma Space Science Laboratory, University of California, Berkeley, USA mb University of Chicago, USA mc Colorado School of Mines, Golden, USA md University of Alabama in Huntsville, Huntsville, USA me University of Wisconsin-Milwaukee, Milwaukee, USA mf NASA - Marshall Space Flight Center, USA mg Vanderbilt University, Nashville, USA 1Corresponding authors: Mario Bertaina (E-mail address: [email protected]), Kenji Shinozaki (E-mail address: [email protected]) Abstract We evaluate the exposure during nadir observations with JEM-EUSO, the Ex- treme Universe Space Observatory, on-board the Japanese Experiment Module of the International Space Station. Designed as a mission to explore the extreme energy Universe from space, JEM-EUSO will monitor the Earth’s nighttime at- mosphere to record the ultraviolet light from tracks generated by extensive air showers initiated by ultra-high energy cosmic rays. In the present work, we dis- cuss the particularities of space-based observation and we compute the annual 3 exposure in nadir observation.
Recommended publications
  • Prototype Design and Mission Analysis for a Small Satellite Exploiting Environmental Disturbances for Attitude Stabilization
    Calhoun: The NPS Institutional Archive Theses and Dissertations Thesis and Dissertation Collection 2016-03 Prototype design and mission analysis for a small satellite exploiting environmental disturbances for attitude stabilization Polat, Halis C. Monterey, California: Naval Postgraduate School http://hdl.handle.net/10945/48578 NAVAL POSTGRADUATE SCHOOL MONTEREY, CALIFORNIA THESIS PROTOTYPE DESIGN AND MISSION ANALYSIS FOR A SMALL SATELLITE EXPLOITING ENVIRONMENTAL DISTURBANCES FOR ATTITUDE STABILIZATION by Halis C. Polat March 2016 Thesis Advisor: Marcello Romano Co-Advisor: Stephen Tackett Approved for public release; distribution is unlimited THIS PAGE INTENTIONALLY LEFT BLANK REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704–0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget, Paperwork Reduction Project (0704-0188) Washington, DC 20503. 1. AGENCY USE ONLY 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED (Leave blank) March 2016 Master’s thesis 4. TITLE AND SUBTITLE 5. FUNDING NUMBERS PROTOTYPE DESIGN AND MISSION ANALYSIS FOR A SMALL SATELLITE EXPLOITING ENVIRONMENTAL DISTURBANCES FOR ATTITUDE STABILIZATION 6. AUTHOR(S) Halis C. Polat 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING Naval Postgraduate School ORGANIZATION REPORT Monterey, CA 93943-5000 NUMBER 9.
    [Show full text]
  • Small Satellite Launch Opportunities
    Small satellites Launch Opportunities Small satellites Deployment from “Kibo” Space Environment and Kibo Utilization Workshop February 9-10, 2017 Hideyuki WATANABE Hiroki AKAGI Japan Aerospace Exploration Agency Human Spaceflight Technology Directorate JEM Mission Operations and Integration Center 1 Small satellites Launch Opportunities by JAXA Deployment from H-IIA launch vehicle Deployment from “Kibo/ISS” JAXA provides opportunities for launching small satellites with the support from technical coordination to launch and deploy for the purposes shown as below: (a) To contribute for easy, fast and on time to launch and operation of small satellites by private enterprises and universities, expanding the application of the space development and capacity building. (b) To promote a technical demonstration by using the small satellites. 2 ISS: Japan’s Capabilities and Contributions ISS Kibo (International Space (Japan Experiment Module) Station) HTV (H-II Transfer Vehicle) . ISS is a huge manned construction located about 400km above the Earth. 15 countries participate in the ISS program . Japan strives to make concrete international contributions through extensive utilization of Kibo and HTV. H-IIB 33 Unique Capability of Kibo – Exposed Facility Kibo has a unique Exposed Facility (EF) with an Airlock (AL) and a Remote Manipulator System (JEMRMS), and has a high capacity to exchange experimental equipment. 44 Unique Capability of Kibo – Exposed Facility Small satellite deployment mission (J-SSOD) Kibo’s unique function: JEM AL (JEM Airlock) and JEMRMS (JEM-Remote Manipulator System) Air Lock JEMRMS (JEM-Remote Manipulator System) JAXA developed the unique system “J-SSOD” (JEM Small Satellite Orbital Deployer) to deploy the satellite and inject the orbit from Kibo.
    [Show full text]
  • H-2 Family Home Launch Vehicles Japan
    Please make a donation to support Gunter's Space Page. Thank you very much for visiting Gunter's Space Page. I hope that this site is useful a nd informative for you. If you appreciate the information provided on this site, please consider supporting my work by making a simp le and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much. H-2 Family Home Launch Vehicles Japan H-2 (ETS 6) [NASDA] H-2 with SSB (SFU / GMS 5) [NASDA] H-2S (MTSat 1) [NASDA] H-2A-202 (GPM) [JAXA] 4S fairing H-2A-2022 (SELENE) [JAXA] H-2A-2024 (MDS 1 / VEP 3) [NASDA] H-2A-204 (ETS 8) [JAXA] H-2B (HTV 3) [JAXA] Version Strap-On Stage 1 Stage 2 H-2 (2 × SRB) 2 × SRB LE-7 LE-5A H-2 (2 × SRB, 2 × SSB) 2 × SRB LE-7 LE-5A 2 × SSB H-2S (2 × SRB) 2 × SRB LE-7 LE-5B H-2A-1024 * 2 × SRB-A LE-7A - 4 × Castor-4AXL H-2A-202 2 × SRB-A LE-7A LE-5B H-2A-2022 2 × SRB-A LE-7A LE-5B 2 × Castor-4AXL H-2A-2024 2 × SRB-A LE-7A LE-5B 4 × Castor-4AXL H-2A-204 4 × SRB-A LE-7A LE-5B H-2A-212 ** 1 LRB / 2 LE-7A LE-7A LE-5B 2 × SRB-A H-2A-222 ** 2 LRB / 2 × 2 LE-7A LE-7A LE-5B 2 × SRB-A H-2A-204A ** 4 × SRB-A LE-7A Widebody / LE-5B H-2A-222A ** 2 LRB / 2 × LE-7A LE-7A Widebody / LE-5B 2 × SRB-A H-2B-304 4 × SRB-A Widebody / 2 LE-7A LE-5B H-2B-304A ** 4 × SRB-A Widebody / 2 LE-7A Widebody / LE-5B * = suborbital ** = under stud y Performance (kg) LEO LPEO SSO GTO GEO MolO IP H-2 (2 × SRB) 3800 H-2 (2 × SRB, 2 × SSB) 3930 H-2S (2 × SRB) 4000 H-2A-1024 - - - - - - - H-2A-202 10000 4100 H-2A-2022 4500 H-2A-2024 5000 H-2A-204 6000 H-2A-212
    [Show full text]
  • A Sample AMS Latex File
    PLEASE SEE CORRECTED APPENDIX A IN CORRIGENDUM, JOSS VOL. 6, NO. 3, DECEMBER 2017 Zea, L. et al. (2016): JoSS, Vol. 5, No. 3, pp. 483–511 (Peer-reviewed article available at www.jossonline.com) www.DeepakPublishing.com www. JoSSonline.com A Methodology for CubeSat Mission Selection Luis Zea, Victor Ayerdi, Sergio Argueta, and Antonio Muñoz Universidad del Valle de Guatemala, Guatemala City, Guatemala Abstract Over 400 CubeSats have been launched during the first 13 years of existence of this 10 cm cube-per unit standard. The CubeSat’s flexibility to use commercial-off-the-shelf (COTS) parts and its standardization of in- terfaces have reduced the cost of developing and operating space systems. This is evident by satellite design projects where at least 95 universities and 18 developing countries have been involved. Although most of these initial projects had the sole mission of demonstrating that a space system could be developed and operated in- house, several others had scientific missions on their own. The selection of said mission is not a trivial process, however, as the cost and benefits of different options need to be carefully assessed. To conduct this analysis in a systematic and scholarly fashion, a methodology based on maximizing the benefits while considering program- matic risk and technical feasibility was developed for the current study. Several potential mission categories, which include remote sensing and space-based research, were analyzed for their technical requirements and fea- sibility to be implemented on CubeSats. The methodology helps compare potential missions based on their rele- vance, risk, required resources, and benefits.
    [Show full text]
  • The First One Hundred Cubesats: a Statistical Look
    Swartwout, M. (2013): JoSS, Vol. 2, No. 2, pp. 213-233 (Peer-reviewed Article available at www.jossonline.com) www.DeepakPublishing.com www.JoSSonline.com The First One Hundred CubeSats: A Statistical Look Michael Swartwout Parks College of Engineering, Aviation and Technology, Saint Louis University, St. Louis, Missouri, USA Abstract The concept of CubeSats was publicly proposed in 2000, with the first CubeSats launched in 2003. By the end of 2012, more than one hundred CubeSats have been launched, and 80 more are manifested for launches in 2013, with at least that many expected in 2014. Ten years ago, CubeSats were routinely dismissed by industry profes- sionals as being too small to be worth flying; now, NASA is the majority launch broker, and a significant share of the manifests are filled by U.S. DoD-sponsored, industry-built CubeSat missions. How did initial perceptions of CubeSats evolve to this state? Are CubeSats toys, tools, or merely another source of orbital debris? With so many CubeSats now in orbit, it is now possible to make a data-based assessment of these missions. Us- ing data collected from a variety of sources, this study evaluates the on-orbit performance of CubeSats. The history of CubeSat missions is reviewed, with the missions classified according to size, origin, mission life, and on-orbit performance. It is shown that several correctable design/implementation errors plague the university side of Cube- Sat missions, and that the P-POD launch container, not the CubeSat specification, is the true enabling technology for this class of mission. Poly-Picosatellite Orbital Deployer (P-POD), a stan- 1.
    [Show full text]
  • Annual Meeting of the Lunar Exploration Analysis Group, P
    Program and Abstract Volume LPI Contribution No. 1685 Annual Meeting of the Lunar Exploration Analysis Group October 22–24, 2012 • Greenbelt, Maryland Sponsor National Aeronautics and Space Administration Conveners Charles Shearer University of New Mexico Jeffrey Plescia The John Hopkins Applied Physics Laboratory Clive Neal University of Notre Dame Stephen Mackwell Lunar and Planetary Institute Scientific Organizing Committee Charles Shearer, University of New Mexico Jeffrey Plescia, John Hopkins University Applied Physics Laboratory Clive Neal, University of Notre Dame Michael Wargo, NASA Headquarters Stephen Mackwell, Lunar and Planetary Institute Dallas Bienhoff, The Boeing Corporation Noah Petro, NASA Goddard Space Flight Center Kurt Sacksteder, NASA Glenn Research Center Greg Schmidt, NASA Lunar Science Institute/NASA Ames Research Center George Tahu, NASA Headquarters Lunar and Planetary Institute 3600 Bay Area Boulevard Houston TX 77058-1113 LPI Contribution No. 1685 Compiled in 2012 by Meeting and Publication Services Lunar and Planetary Institute USRA Houston 3600 Bay Area Boulevard, Houston TX 77058-1113 This material is based upon work supported by NASA under Award No. NNX08AC28A. Any opinions, findings, and conclusions or recommendations expressed in this volume are those of the author(s) and do not necessarily reflect the views of the National Aeronautics and Space Administration. The Lunar and Planetary Institute is operated by the Universities Space Research Association under a cooperative agreement with the Science Mission Directorate of the National Aeronautics and Space Administration. Material in this volume may be copied without restraint for library, abstract service, education, or personal research purposes; however, republication of any paper or portion thereof requires the written permission of the authors as well as the appropriate acknowledgment of this publication.
    [Show full text]
  • Small-Satellite Mission Failure Rates
    NASA/TM—2018– 220034 Small-Satellite Mission Failure Rates Stephen A. Jacklin NASA Ames Research Center, Moffett Field, CA March 2019 This page is required and contains approved text that cannot be changed. 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 in or other meetings sponsored or helping NASA maintain this important role. co-sponsored by NASA. The NASA STI program operates under the SPECIAL PUBLICATION. Scientific, auspices of the Agency Chief Information Officer. technical, or historical information from It collects, organizes, provides for archiving, and NASA programs, projects, and missions, disseminates NASA’s STI. The NASA STI often concerned with subjects having program provides access to the NTRS Registered substantial public interest. and its public interface, the NASA Technical Reports Server, thus providing one of the largest TECHNICAL TRANSLATION. collections of aeronautical and space science STI English-language translations of foreign in the world. Results are published in both non- scientific and technical material pertinent to NASA channels and by NASA in the NASA STI NASA’s mission. Report Series, which includes the following report types: Specialized services also include organizing and publishing research results, distributing TECHNICAL PUBLICATION. Reports of specialized research announcements and completed research or a major significant feeds, providing information desk and personal phase of research that present the results of search support, and enabling data exchange NASA Programs and include extensive data services.
    [Show full text]
  • Microgravity Playscapes Play in Long-Term Space Missions S M L E A
    Microgravity Playscapes Play in Long-Term Space Missions s M L E A e authors examine the potential impact of play on astronauts adapting to the extreme conditions of space travel. ey cite research showing that welltrained astronauts, though in general physically t and emotionally stable, can suer from—among other things—boredom and sensory deprivation in the connes of the microgravity capsules of space ight. Astronauts on duty, the authors argue, are overscheduled, understimulated, isolated, and—importantly—play deprived. Introducing play into space ight routines, they contend, keeps astronauts saner, boosts their morale, and provides leisuretime pleasure. ey discuss the impor- tance of play and its uses in Ackermann’s Whole Child Development Guide, which, they argue, is also suitable for adult space travelers. And they provide guidelines for designing a playscape in microgravity that taps the unique, inherently playful qualities of weightlessness itself. Key words: Microgravity Playscape Adaptation approach ; play and astronauts; playscapes in microgravity; space travel and play Introduction S has long captured the human imagination. e very notion of breaking away from the Earth’s ultimate constraint of gravity and oating around in weightlessness is inherently playful. Hence the attraction—not just to children but, increasingly, to grown-ups—to embark! Yet, scientists report that living and working for long periods in a conned, isolated microgravity habitat take a toll on those real space travelers, astronauts. In this article, we suggest that play alleviates the boredom, sensory deprivation, connement, isolation, apathy, and conict that make up life in a crowded capsule beyond Earth’s orbit. Levitating in a man-made station adri in space epitomizes the displacements and disorientation characteristic of play.
    [Show full text]
  • Committee on the Peaceful Uses of Outer Space
    United Nations COPUOS/LEGAL/T.820 Committee on the Peaceful Unedited transcript Uses of Outer Space Legal Subcommittee th 820 Meeting Monday, 28 March 2011, 10 a.m. Vienna Chairman: Mr. A. Talebzadeh (Islamic Republic of Iran) The meeting was called to order at 10.12 a.m. _____(?) achievements the Committee and the Legal Subcommittee have been instrumental in the The CHAIRMAN Excellencies, development of an international legal regime governing distinguished delegates, ladies and gentlemen, good the activities of States in the exploration and use of morning. I am delighted and honoured to welcome you outer space concerning five treaties and five sets of all to the Vienna International Centre and now declare declaration and principle on outer space activities. open the fiftieth session and 820th meeting of the Among them the Outer Space Treaty of 1967 Legal Subcommittee of the United Nations Committee represented a landmark in legal instruments, the Magna on the Peaceful Uses of Outer Space. Carta of space law. The Outer Space Treaty together with the other core treaties on outer space form the Today we are taking part in a remarkable legal order for today’s space activities. It is with great event as our Subcommittee is holding its fiftieth pleasure I witnessed the effort of the Committee and session. Moreover, this year will also bring another the Legal Subcommittee to further advance the impressive communication, the fiftieth anniversary of application of the legal regime of outer space and to the main committee. Please allow me to make a brief promote capacity building in space law.
    [Show full text]
  • The Future of Cubesat Communications
    The Future of CubeSat Data Communications Bryan Klofas KF6ZEO SRI International [email protected] AMSAT-NA Symposium Orlando, Florida 26 October 2012 CubeSat Launches (1 of 3) • Eurockot Launch (30 June 2003) • Minotaur 1 (11 Dec 2006) Green = Amateur – AAU1 CubeSat – GeneSat-1 (2.4GHz) Red = Experimental – DTUsat-1 (DOA) • Dnepr Launch 2 (17 Apr 2007) Blue = Non-Amateur – CanX-1 (DOA) – CSTB1 – Cute-1 (CO-55) – AeroCube-2 – QuakeSat-1 – CP4 – XI-IV (CO-57) – Libertad-1 • SSETI Express (27 Oct 2005) – CAPE1 – XI-V (CO-58) – CP3 – NCube-2 (DOA) – MAST – UWE-1 • PSLV-C9 (28 Apr 2008) • M-V-8 Launch (22 Feb 2006) – Delfi-C3 (DO-64) – Cute-1.7+APD (CO-56) – SEEDS-2 (CO-66) • Dnepr Launch 1 (26 July 2006) – CanX-2 (launch failure) – AAUSAT-II – Compass-1 • Falcon Launch 1 (2 Aug 2008) (launch failure) Slide 2 CubeSat Launches (2 of 3) • Minotaur-1 (19 May 2009) • STP-S26 (19 Nov 2010) Green = Amateur – AeroCube-3 – RAX-1 (2.4 GHz) Red = Experimental – CP-6 – O/ORES (2.4 GHz) Blue = Non-Amateur – HawkSat-1 (DOA) – NanoSail-D2 – PharmaSat (2.4 GHz) • Falcon 9-002 (8 Dec 2010) • ISILaunch 01 (23 Sep 2009) – Perseus (4) – BEESAT – QbX (2) – UWE-2 – SMDC-ONE – ITUpSAT1 – Mayflower (437 MHz) – SwissCube • ELaNa-1/Taurus XL (4 Mar 2011) • Japanese H-IIA F17 (20 May 2010) (launch failure) – K-Sat • PSLV-C18 (12 Oct 2011) – Waseda-SAT2 – Jungu – Negai Star • PSLV-C15 (12 July 2010) – TIsat-1 – STUDSAT Slide 3 CubeSat Launches (3 of 3) • ELaNa-3/NPP (28 Oct 2011) • ELaNa-6/NROL-36 (13 Sep 2012) Green = Amateur – M-Cubed – SMDC-ONE (2) Red = Experimental
    [Show full text]
  • Commercial Space Transportation: 2012 Year in Review
    Federal Aviation Administration COMMERCIAL SPACE TRANSPORTATION: 2012 YEAR IN REVIEW JANUARY 2013 2012 Year in Review About the 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 web site at http://www.faa.gov/about/office_org/headquarters_offices/ast/. Cover: Art by John Sloan (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 / Office of Commercial Space Transportation CONTENTS INTRODUCTION. 1 EXECUTIVE SUMMARY ............................................2 2012 LAUNCH ACTIVITY . 3 WORLDWIDE ORBITAL LAUNCH ACTIVITY. 3 Worldwide Launch Revenues. 6 Worldwide Orbital Payload Summary ................................. 7 Commercial Launch Payload Summary . 8 Non-Commercial Launches ......................................... 9 U.S. AND FAA-LICENSED ORBITAL LAUNCH AND REENTRY ACTIVITY . 10 FAA-Licensed Orbital Launch Summary .............................. 10 FAA Reentry License Summary ..................................... 11 NON-U.S.
    [Show full text]
  • Evaluation of Radiation Tolerant Satellite Communication Modem
    Master Thesis Electrical Engineering June 2012 Evaluation of radiation tolerant satellite communication modem Venkata Srikanth Bhuma Santosh Kumar Balsu School of Computing Blekinge Institute of Technology 371 79 Karlskrona Sweden This thesis is submitted to the School of Computing at Blekinge Institute of Technology in partial fulfillment of the requirements for the degree of Master of Science in Electrical Engineering. The thesis is equivalent to 20 weeks of full time studies. Contact Information: Author(s): Venkata Srikanth Bhuma E-mail: [email protected] Santosh Kumar Balsu E-mail: [email protected] External advisor(s): Jan Schulte ÅAC Microtec AB Dag Hammarskjölds väg 54, SE-751 83 Uppsala Sweden Phone: +46700910429 University advisor(s): Craig A. Lindley School of Computing University Examiner(s): Patrik Arlos School of Computing School of Computing Internet : www.bth.se/com Blekinge Institute of Technology Phone : +46 455 38 50 00 371 79 Karlskrona Fax : +46 455 38 50 57 ii Sweden ABSTRACT The design specification of CubeSat standards by California Polytechnique University has become a major milestone in development and deployment of nano satellites. The number of CubeSats that are being deployed into the orbit has increased in recent years. The design and development have been transformed from traditional hardware devices to software defined radios. However there is a lack of clear understanding and concrete findings on developing proper communication transceivers. The lack of knowledge of proper guidelines to be followed to design and develop communication subsystems prompts and acts as a base for us in understanding the communication subsystem design standards followed by CubeSat projects in various universities.
    [Show full text]