Committee on the Peaceful Uses of Outer Space
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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. -
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. -
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 -
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. -
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. -
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. -
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. -