Tech Bytes Fall 2017
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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. -
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. -
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. -
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. -
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. -
Miguel Yagües Palazón Ph.D
Journal of the Spanish Institute for Strategic Studies ISSN-e: 2255-3479 Miguel Yagües Palazón Ph.D. in International Security. Instituto General Gutiérrez Mellado (UNED). E-mail: [email protected] ENVIRONMENTAL CHALLENGES IN OUTER SPACE IN THE FRAMEWORK OF THE SECOND SPACE AGE Abstract The second space age (1991-present) is distinguished by two charac- teristics: the difficulty in reaching space governance agreements with emerging geopolitical actors, unlike the first space age (1957-1990) du- ring which the entire space regulatory framework was structured; and the advent of numerous new public and private space actors –especially from 2010 onwards– triggering a corresponding increase in space acti- vities in order to benefit from space applications such as reconnaissance activities, communications, space positioning systems and meteorology. These two factors are directly affecting the fragile space environment, and placing its sustainability at risk. In the absence of an international regulatory framework, the adoption of national laws is presented here as an alternative means of ensuring the responsible management of the space environment. Keywords Space environment; space sustainability; second space age; space gover- nance; new space actors; space debris. To quote this article: YAGÜES, M. “Environmental Challenges in Outer Space in the Fra- mework of the Second Space Age”. Journal of the Spanish Institute for Strategic Studies. 2018, n.º 12, pp. Revista del Instituto Español de Estudios Estratégicos n.º 12 - Año: 2018 - Págs.: 397 a 431 397 Journal of the Spanish Institute for Strategic Studies Núm. 12 / 2018 THE TRANSITION FROM THE FIRST TO THE SECOND SPACE AGE he 1960s and 1970s laid the foundations for current space governance, foste- red by the commitment of the United States and the former Soviet Union to Tmaintaining strategic stability. -
ミルスペース 121011------[What’S New in Virtual Library?]
9- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - -ミルスペース 121011- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - [What’s New in Virtual Library?] McGrawHill AW&ST Aviation Week AFA AFM AirForce Magazine 120924AWST_Contents.pdf, Cover.jpg 1210AFM_Cover.jpg AIAA Aerospace America 1209AFM_Cover.jpg 1210AeroAme_Contents.pdf, Cover.jpg 1208AFM_Cover.jpg 1209AeroAme_Cover-s.jpg Milsatmagazine 1207&08AeroAme_Cover-ss.jpg milsatmagazine_12Sept_Contents.pdf, Cover.jpg 1206AeroAme_Contents.pdf, Cover.jpg ESA ESA Bulletin Milbank Space Business Review 1208ESA_Bull151_92pages.pdf, Cover.jpg 1209_Space_Business_Review.pdf 1208ESA_Bull151_Contents.pdf TIROS Space Information JAXA 空と宙 1210TIROS_Space_Info_6pages.pdf, Cover.jpg 1209&10Sora-To-Sora_no49_8pages.pdf, Cover.jpg 1209TIROS_Space_Info_6pages.pdf, Cover.jpg NICT NICT News NASA MSFC MarshallStar 1209NICT_News_12pages.pdf, Cover.jpg 121003MarshallStar_Cover.jpg 1208NICT_News_12pages.pdf, Cover.jpg 120926MarshallStar_Cover.jpg [What’s New in Real Library?] [謝辞] JAXA より ISAS ニュース 12.09 No.378 寄贈、航空図書館より Military Technology 12.09 寄贈、感謝。 - - - - - - - - - - - - - - - - - - - -Futron 12.10 - - - - - - - - - - - - - - - - - - - - - - - 1 2012 Orbital Launches by Launch Vehicle Family 2012 Orbital Commercial Launches Manufacturer Market Share of Satellites Launched Through September 30, 2012 2012 Cumulative 36-MHz Transponder Equivalents Launched by Frequency 2 Selected Satellites with Regulatory Activity During September 2012 Satellite Location Activity SES-4 22WL The FCC granted SES' request to add the SES-4 satellite at 22 WL to the FCC's Permitted Space Station List. Echo-45W 45.1WL EchoStar Satellite Operating Corporation (ESOC) applied to launch and operate ECHO-45W at 45.1 WL in order to provide BSS to Brazilian customers. Galaxy 12 129WL The FCC granted Intelsat's request to relocate Galaxy 12 from 132.9 WL to 129 WL. DIRECTV 1R 304.2WL DIRECTV applied to operate DIRECTV 1R at 304.2WL (55.8 EL) instead of the original 303.84 WL (56.16 EL) location. -
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 -
WORLD SPACECRAFT DIGEST by Jos Heyman 2013 Version: 1 January 2014 © Copyright Jos Heyman
WORLD SPACECRAFT DIGEST by Jos Heyman 2013 Version: 1 January 2014 © Copyright Jos Heyman The spacecraft are listed, in the first instance, in the order of their International Designation, resulting in, with some exceptions, a date order. Spacecraft which did not receive an International Designation, being those spacecraft which failed to achieve orbit or those which were placed in a sub orbital trajectory, have been inserted in the date order. For each spacecraft the following information is provided: a. International Designation and NORAD number For each spacecraft the International Designation, as allocated by the International Committee on Space Research (COSPAR), has been used as the primary means to identify the spacecraft. This is followed by the NORAD catalogue number which has been assigned to each object in space, including debris etc., in a numerical sequence, rather than a chronoligical sequence. Normally no reference has been made to spent launch vehicles, capsules ejected by the spacecraft or fragments except where such have a unique identification which warrants consideration as a separate spacecraft or in other circumstances which warrants their mention. b. Name The most common name of the spacecraft has been quoted. In some cases, such as for US military spacecraft, the name may have been deduced from published information and may not necessarily be the official name. Alternative names have, however, been mentioned in the description and have also been included in the index. c. Country/International Agency For each spacecraft the name of the country or international agency which owned or had prime responsibility for the spacecraft, or in which the owner resided, has been included.