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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. -
Chinese Spacecraft En Route to Orbiting Module 17 June 2012
Chinese spacecraft en route to orbiting module 17 June 2012 everything is going according to plan," China Central Television said in its midday news program. Two of the astronauts will live and work inside the module while the third remains in the capsule in case of emergency. The astronauts are to conduct medical tests and other experiments before returning to Earth. Shenzhou 9 spacecraft rocket launches from the Jiuquan Satellite Launch Center in Jiuquan, China, Saturday, June 16, 2012. China sent its first woman and two other astronauts into space Saturday to work on a temporary space station for about a week, in a key step toward becoming only the third nation to set up a permanent base in orbit. (AP Photo/Ng Han Guan) (AP) - A spacecraft carrying China's first female China's first female astronaut Liu Yang salutes during a astronaut and two male crew mates made a sending off ceremony as she departs for the Shenzhou 9 planned course change Sunday en route to spacecraft rocket launch pad at the Jiuquan Satellite docking with an orbiting module, state television Launch Center in Jiuquan, China, Saturday, June 16, reported. 2012. China will send its first woman and two other astronauts into space Saturday to work on a temporary space station for about a week, in a key step toward The Shenzhou 9 capsule was launched Saturday becoming only the third nation to set up a permanent on China's most ambitious space mission yet in a base in orbit.(AP Photo/Ng Han Guan) step toward building a permanent space station. -
Techedsat Satellite Project Techedsat Formal Orbital Debris
TechEdSat Satellite Project TES-03-XS008 Orbital Debris Assessment Report (ODAR) Rev A TechEdSat Formal Orbital Debris Assessment Report (ODAR) In accordance with NPR 8715.6A, this report is presented as compliance with the required reporting format per NASA-STD-8719.14, APPENDIX A. Report Version: A (4/2/2012) DAS Software Used in This Analysis: DAS v2.0 Page 1 of 34 TechEdSat Satellite Project TES-03-XS008 Orbital Debris Assessment Report (ODAR) Rev A Page 2 of 34 TechEdSat Satellite Project TES-03-XS008 Orbital Debris Assessment Report (ODAR) Rev A Record of Revisions Affected Description of Rev Date Author (s) Pages Change Ali Guarneros Luna, A 4/2/2012 All Initial Release Christopher Hartney, Page 3 of 34 TechEdSat Satellite Project TES-03-XS008 Orbital Debris Assessment Report (ODAR) Rev A Table of Contents Self-assessment and OSMA assessment of the ODAR using the format in Appendix A.2 of NASA-STD-8719.14: Assessment Report Format Mission Description ODAR Section 1: Program Management and Mission Overview ODAR Section 2: Spacecraft Description ODAR Section 3: Assessment of Spacecraft Debris Released during Normal Operations ODAR Section 4: Assessment of Spacecraft Intentional Breakups and Potential for Explosions. ODAR Section 5: Assessment of Spacecraft Potential for On-Orbit Collisions ODAR Section 6: Assessment of Spacecraft Postmission Disposal Plans and Procedures ODAR Section 7: Assessment of Spacecraft Reentry Hazards ODAR Section 8: Assessment for Tether Missions Appendix A: Acronyms Appendix B: Battery Data Sheet Appendix C: Wiring Schematics Page 4 of 34 TechEdSat Satellite Project TES-03-XS008 Orbital Debris Assessment Report (ODAR) Rev A Selfassessment and OSMA assessment of the ODAR using the format in Appendix A.2 of NASASTD8719.14: A self assessment is provided below in accordance with the assessment format provided in Appendix A.2 of NASA-STD-8719.14. -
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. -
Operation Results of Cubesat RAIKO Released from International Space Station
Operation Results of Cubesat RAIKO Released from International Space Station 1) 1) 1) 1) 1) By Yuji SAKAMOTO , Yuta TANABE , Hitoshi YAGISAWA , Nobuo SUGIMURA , Kazuya YOSHIDA , 2) 3) 4) Masanori NISHIO , Tomoyuki NAKAJO , and Hiroaki AKIYAMA 1) Department of Aerospace Engineering, Tohoku University, Sendai, Japan 2) Department of Physics and Space, Kagoshima University, Kagoshima, Japan 3) Department of Electrical, Electronic and Computer Engineering, Fukui University of Technology, Fukui, Japan 4) Institute for Education on Space, Wakayama University, Wakayama, Japan The 2-unit size cubesat RAIKO is the nanosatellite developed by Tohoku University and Wakayama University. This paper shows the mission and system specifications. The satellite was released to space on October 4, 2012 from International Space Station, which was the 419-km alt. circular orbit. The techniques for 50-kg microsatellites by Tohoku University are transferred to this satellite, so a lot of functions are included although the power and mass budgets are strongly restricted. The primary missions are the photo storage by different 3 optical sensors, the de-orbit mechanism experiment by expandable thin films, and Ku-band downlink communication experiment. The satellite operation was finished by orbital decay on August 6, 2013. The telemetry data were successful received in total 123 passes, in which total 63 photo images were obtained and maximum 100 kbps (200 ksps) downlink was successful. Using color CMOS camera, gradually separating ISS could be confirmed. From the analysis result of house-keeping data, the solar generation power in sunshine was 3.38 W (no paddles) to 5.77 W (with paddles) in average, the temperature of onboard computer was in the range of 20.8 to 28.7 degC, and the battery temperature was 4.2 degC in average. -
Cubesat-Services.Pdf
Space• Space Station Station Cubesat CubesatDeployment Services Deployment Services NanoRacks Cubesat Deployer (NRCSD) • 51.6 degree inclination, 385-400 KM • Orbit lifetime 8-12 months • Deployment typically 1-3 months after berthing • Soft stowage internal ride several times per year Photo credit: NASA NRCSD • Each NRCSD can deploy up to 6U of CubeSats • 8 NRCSD’s per airlock cycle, for a total of 48U deployment capability • ~2 Air Lock cycles per mission Photo Credit: NanoRacks LLC Photo credit: NASA 2. Launched by ISS visiting vehicle 3. NRCSDs installed by ISS Crew 5. Grapple by JRMS 4. JEM Air Lock depress & slide 6. NRCSDs positioned by JRMS table extension 1. NRCSDs transported in CTBs 7. Deploy 8. JRMS return NRCSD-MPEP stack to slide table; 9. ISS Crew un-install first 8 NRCSDs; repeat Slide table retracts and pressurizes JEM air lock install/deploy for second set of NRCSDs NanoRacks Cubesat Mission (NR-CM 3 ) • Orbital Sciences CRS-1 (Launched Jan. 9, 2014) • Planet Labs Flock1A, 28 Doves • Lithuanian Space Assoc., LitSat-1 • Vilnius University & NPO IEP, LituanicaSat-1 • Nanosatisfi, ArduSat-2 • Southern Stars, SkyCube • University of Peru, UAPSat-1 Photo credit: NASA Mission Highlights Most CubeSats launched Two countries attain in a single mission space-faring status World’s largest remote Kickstarter funding sensing constellation • NR-CM3 • Orbital Science CRS-1, Launch Jan 9, 2014 • Air Lock Cycle 1, Feb 11-15, 2014 Dove CubeSats • Deployers 1-8 (all Planet Labs Doves) Photo credit: NASA • NR-CM3 • Orbital Science CRS-1, -
2020 Spring GOES DCS Technical Working Group (TWG) 125 Meeting Th Tuesday, May 5 , 2020 (Virtual Via Webex and Teleconference)
th 2020 Spring GOES DCS Technical Working Group (TWG) 125 Meeting th Tuesday, May 5 , 2020 (Virtual Via Webex and Teleconference) Opening Remarks/ Introductions – LySanias Broyles (STIWG Chair and U.S. Army Corps of Engineer, Rock Island District) and Richard Antoine (NESDIS/OSPO/SPSD/Direct Services Branch) Richard Antoine opened the meeting at 09:30. DCS Update: 100 BPS Discontinuation, CS2 Status (Richard Antoine (NESDIS/OSPO/SPSD/ Direct Services Branch) Richard began by noting that we now have 659 SUAs and 2,134 registered users. Also noted was that the 100 BPS DCPs are no longer supported as of last January 21, 2020. There has also been an enhancement to DAMS-NT that should result in a better service to users by adding enhanced message statistics and that the site surveys needed to install a backup pilot at the CBU in Fairmont, WB have been accomplished. Letecia Reeves then went over the chart below showing the status of all the DCPs in the system. DCP Status 100 Baud 300 Baud 1200 Baud Totals Active DCPs 0 29,304 520 29,824 Inactive DCPs 0 7,347 604 7,951 Unused DCPs 0 2,400 214 2,614 Totals 0 39,051 1,338 40,389 Note: Statistics do not include the parked channel (-1). Letecia then discussed the factors that determine the status of the DCP. The status levels are in column one, on the left in the table above. They factors are listed in bullet form below: ● A: System received data transmissions w/in 2 days. ● D: No data transmission received in 2 days. -
In This Issue
Vol. 41 No.9, June 2016 Editor: Jos Heyman FBIS In this issue: Astronaut Log (2009-2015) 5 Cancelled Projects: HOPE and HOPE-X 2 HOPE TIROS SPACE INFORMATION Cancelled Projects: HOPE and HOPE-X 86 Barnevelder Bend, Southern River WA 6110, Australia Tel + 61 8 9398 1322 (e-mail: [email protected]) By Jos Heyman The Tiros Space Information (TSI) - News Bulletin is published to promote the scientific exploration and In 1986 Japan began the development of the H2 Orbiting Plane (HOPE), a re-usable space plane commercial application of space through the dissemination of current news and historical facts. that would carry up to four astronauts to the Freedom space station in which Japan had agreed to In doing so, Tiros Space Information continues the traditions of the Western Australian Branch of the take part. It was one of Japan’s two contributions to the Freedom Space Station operations, the Astronautical Society of Australia (1973-1975) and the Astronautical Society of Western Australia (ASWA) other one being the Japanese Experiment Module (JEM) which eventually evolved into the Kibo (1975-2006). module of the International Space Station (ISS). The News Bulletin can be received worldwide by e-mail subscription only. Subscriptions can be requested by sending an e-mail address to [email protected]. Tiros Space Information reserves the right to refuse any subscription request without the need to provide a reason. All opinions expressed are those of the authors and do not necessarily reflect the opinions of the Editor or Tiros Space Information. All material contained in this publication may be reproduced provided due acknowledgment is made. -
Possibilities and Future Vision of Micro/Nano/Pico-Satellites - from Japanese Experiences
CanSat & Rocket Experiment(‘99~) Hodoyoshiハイブリッド-1 ‘14 ロケット Possibilities and Future Vision of Micro/nano/pico-satellites - From Japanese Experiences Shinichi Nakasuka University of Tokyo PRISM ‘09 CubeSat 03,05 Nano-JASMINE ‘15 Contents • Features of Micro/nano/pico-satellites • Japanese History and Lessons Learned – CanSat to CubeSat “First CubeSat on orbit” – From education to practical applications – Important tips for development • Visions on Various Applications of Micro/nano/pico-satellites • University Space Engineering Consortium (UNISEC) and International Collaborations Micro/nano/pico-satellite “Lean Satellite” Micro-satellite: 20-100kg Nano-satellite: 2-20kg Pico-satellite: 0.5-2kg Japanese Governmental Satellites ALOS-1: 4 ton ASNARO: 500 kg Kaguya: 3 ton Hayabusa: 510 kg Motivation of Smaller Satellites Current Problem of Mid-large Satellites ALOS 4.0 (4t) Trend towards 3.5 larger satellites Weight SELENE ・Enormous cost >100M$ 3.0 (3t) ・Development period >5-10 years 2.5 ・Conservative design (ton 2.0 ・Almost governmental use ・No new users and utilization ideas ) ・Low speed of innovation 1.5 10-50M$ Micro 1.0 Small-sat /Nano /Pico 0.5 Sat 0 1975 1980 1985 1990 1995 2000 2005 <50kg Introduce more variedGEO new players intoOTHERS space. 1-5M$ Innovation by Micro/nano/pico satellites (<100kg) 超小型衛星革命 Education Remote sensing Telescope Weather Bio-engineering Re-entry Rendezvous/ Communication Space Science Atmosphere Exploration High Resolution. docking Universty/venture companies’ innovative idea and development process <10M$ -
CASC Efforts on Dealing with Space Debris Toward Space Long Term Sustainability
China Aerospace Science and Technology Corporation CNSACNSA CASC Efforts on Dealing with Space Debris toward Space Long Term Sustainability Dr. Zizheng GONG Chief Scientist Beijing Institute of Spacecraft Environment Engineering, China Aerospace Science and Technology Corporation (CASC) COPUOS Scientific and Technical Subcommittee, the fifty session. Vienna, February 11-22,2013. Slide 1 Outline CNSACNSA 1 Overview 2 CASC Efforts of Space Debris Activities 3 Views and Conclusions COPUOS Scientific and Technical Subcommittee, the fifty session. Vienna, February 11-22,2013. Slide 2 CONTENTS CNSACNSA 1 Overview 2 CASC Efforts of Space Debris Activities 3 Conclusions and Comments COPUOS Scientific and Technical Subcommittee, the fifty session. Vienna, February 11-22,2013. Slide 3 China Aerospace Science and Technology Corporation CNSACNSA CASC is the main and the largest state-owned aerospace enterprise in China. Main fields & Mission : 1. Launchers 2. Human Spaceflight 3. Earth Observation 4. Telecommunications 5. Navigation 6. Space Science and Deep Space Exploration COPUOSFeb Scientific 14,2013 Viennaand Technical Subcommittee, the fifty session. Vienna, February 11-22,2013. SlideSlide 4 4 Manned Space Programs CNSACNSA The current manned space program in China Programs: is composed of 3 phases: Shenzhou - 1 Shenzhou - 2 Phase 1: Manned space flight Shenzhou - 3 Phase 2:Extravehicular activity, rendezvous & docking Shenzhou - 4 Shenzhou - 5 Phase 3: Space Lab and Space station Shenzhou - 6 In 2011 and 2012, Tiangong-1 and Shenzhou-8, Shenzhou-9 Shenzhou - 7 accomplished first space rendezvous and docking test, laying Tiangong - 1 the foundation for the construction of future space station. Shenzhou - 8 Shenzhou - 9 Extravehicular activity Rendezvous & Docking Space Lab Feb 14,2013 Vienna COPUOS Scientific and Technical Subcommittee, E-mail:[email protected] the fifty session. -
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. -
Space Security Index 2013
SPACE SECURITY INDEX 2013 www.spacesecurity.org 10th Edition SPACE SECURITY INDEX 2013 SPACESECURITY.ORG iii Library and Archives Canada Cataloguing in Publications Data Space Security Index 2013 ISBN: 978-1-927802-05-2 FOR PDF version use this © 2013 SPACESECURITY.ORG ISBN: 978-1-927802-05-2 Edited by Cesar Jaramillo Design and layout by Creative Services, University of Waterloo, Waterloo, Ontario, Canada Cover image: Soyuz TMA-07M Spacecraft ISS034-E-010181 (21 Dec. 2012) As the International Space Station and Soyuz TMA-07M spacecraft were making their relative approaches on Dec. 21, one of the Expedition 34 crew members on the orbital outpost captured this photo of the Soyuz. Credit: NASA. Printed in Canada Printer: Pandora Print Shop, Kitchener, Ontario First published October 2013 Please direct enquiries to: Cesar Jaramillo Project Ploughshares 57 Erb Street West Waterloo, Ontario N2L 6C2 Canada Telephone: 519-888-6541, ext. 7708 Fax: 519-888-0018 Email: [email protected] Governance Group Julie Crôteau Foreign Aairs and International Trade Canada Peter Hays Eisenhower Center for Space and Defense Studies Ram Jakhu Institute of Air and Space Law, McGill University Ajey Lele Institute for Defence Studies and Analyses Paul Meyer The Simons Foundation John Siebert Project Ploughshares Ray Williamson Secure World Foundation Advisory Board Richard DalBello Intelsat General Corporation Theresa Hitchens United Nations Institute for Disarmament Research John Logsdon The George Washington University Lucy Stojak HEC Montréal Project Manager Cesar Jaramillo Project Ploughshares Table of Contents TABLE OF CONTENTS TABLE PAGE 1 Acronyms and Abbreviations PAGE 5 Introduction PAGE 9 Acknowledgements PAGE 10 Executive Summary PAGE 23 Theme 1: Condition of the space environment: This theme examines the security and sustainability of the space environment, with an emphasis on space debris; the potential threats posed by near-Earth objects; the allocation of scarce space resources; and the ability to detect, track, identify, and catalog objects in outer space.