Orbital Debris Quarterly News 22-1

Total Page:16

File Type:pdf, Size:1020Kb

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. 36100 Debris fragments have been 240 ] ° Charts by Number 36000 altitude [ observed in the vicinity and Mass 10 of the AMC-9 spacecraft. 180 35900 SES has regained control [km] longitude Space Missions of the spacecraft and has 35800 120 and Satellite transferred AMC-9 to the so-called graveyard 35700 Box Score 12 subsatellite orbit, a long-term disposal 60 subsatellite longitude [o] orbit region located apogee alt [km] 35600 above the GEO belt. The perigee alt. [km] 0 35500 NASA Orbital Debris Program Office (ODPO) 2017.00 2017.08 2017.17 2017.25 2017.33 2017.42 2017.50 2017.58 2017.67 2017.75 2017.83 2017.92 2018.00 characterizes this episode time [YYYY.Y] as an anomalous event. Figure 1. The 2017 orbital evolution of the AMC-9 spacecraft. Depicted are the subsatellite longitude, The spacecraft bus is demonstrating a westward drift post-event, and the apogee/perigee altitude history. The altitude A publication of the popular Thales Alenia profile clearly indicates the abrupt nature of the 17 June 2017 event, recovery activities by the owner/ the NASA Orbital Space (formerly Alcatel operator, and the final boost to the so-called graveyard orbit above the GEO belt. Inclination control Debris Program Office Space) Spacebus-3000B3 appears to have terminated in late June 2017. Orbital Debris Quarterly News Events in GEO continued from page 1 10:43 GMT on 26 August, TELKOM-1 was in a TELKOM‐1 (SSN 25880, 1999‐042A) 120 36000 35793 x 35781 km, 0.0112° orbit; afterwards, at approximately 19:36 GMT on 29 August, the 35950 orbit was 35838 x 35764 km at an inclination 35900 of 0.0237°. PT Telkom, the spacecraft owner- 110 operator, declared on 30 August that the spacecraft 35850 could not be salvaged [1]. Following this event, ] the spacecraft began a westward drift in the GEO ° altitude [ 35800 belt. As this ODQN goes to press, the spacecraft orbit has evolved as depicted in Fig. 2. The 100 35750 [km] NASA Orbital Debris Program Office (ODPO) longitude 35700 characterizes this episode as an anomalous event. The spacecraft bus is the Lockheed Martin 35650 A2100 platform. Spacecraft dry mass is estimated 90 to be on the order of 1640 kg. On-board stored subsatellite 35600 subsatellite longitude [o] energy sources include fuel and pressurized apogee alt [km] 35550 components as well as the battery subsystem. perigee alt. [km] 80 35500 Reference 1. “Antenna glitch disconnects Telkom-1 satellite customers in Indonesia,” http:// 2017.00 2017.08 2017.17 2017.25 2017.33 2017.42 2017.50 2017.58 2017.67 2017.75 2017.83 2017.92 2018.00 spacenews.com/antenna-glitch-disconnects- time [YYYY.Y] telkom-1-satellite-customers-in-indonesia/ when Figure 2. The 2017 orbital evolution of the TELKOM-1 spacecraft. Depicted are the subsatellite longitudes, demonstrating accessed December 2017. ♦ a westward drift post-event, and the apogee/perigee altitude history. The altitude profile clearly indicates the abrupt nature of the event and possible mitigation activities by the owner/operator. Inclination control apparently terminated in early September 2017. Space Debris Sensor Launches Aboard SpaceX-13 The NASA Orbital Debris Program Office at the ESA Columbus module’s External Payload press, to commence 3 years of operations at (ODPO) Space Debris Sensor (SDS) was Facility-Starboard Overhead-X (EPF-SOX) this location. Following completion of the SDS launched to the International Space Station (ISS) mission, the SDS is planned to be disposed of aboard the Commercial Resupply mission CRS- by reentry aboard a future CRS-series mission. 13 (or SpaceX-13, SpX-13) vehicle on Friday, TIC GRID ORB The SDS is the first flight demonstration COUS ITAL N 15 December 2017, from Cape Canaveral E/A AS of the Debris Resistive/Acoustic Grid TIV A-N Air Force Station's (CCAFS's) Launch IS AV Orbital NASA-Navy Sensor (DRAGONS) ES Y Complex 40. Following the launch of a R S developed and matured by the NASA E Space Exploration Technologies Corp. IS N ODPO [1]. The DRAGONS concept R S (SpaceX) Falcon 9 recoverable booster, B O combines several technologies E R Fig. 1, the Dragon vehicle separated D to characterize the size, speed, from the Falcon 9’s second stage, direction, and density of small Fig. 2, en route to the ISS. The launch impacting objects. With a minimum featured, for the first time, the second 3-year operational lifetime, the SDS use of both the Falcon 9 first stage and is anticipated to collect statistically the Dragon capsule, and post-staging significant information on orbital the Falcon 9 first stage landed at SpaceX's debris ranging from 50 µm to 500 µm Landing Zone 1 at CCAFS. The Dragon IS R in size. Most impacts will be around the S D SO capsule rendezvoused with the ISS on Sunday, RAG SEN threshold of 50 µm; the estimated number of 17 December, and was captured and docked that ONS SPACE DEBRIS 500 µm and larger impacts for a square meter day. in an ISS orbit over 2018-2020 is 0.84. The The SDS was robotically extracted from development of the SDS has been chronicled the SpX-13 Dragon trunk and installed on location. Following a multi-week checkout 1 January 2018. As seen in Fig. 3, the SDS is hosted period SDS is expected, as the ODQN goes to continued on page 3 2 www.orbitaldebris.jsc.nasa.gov SDS Launches continued from page 2 in the ODQN (ODQN vol. 21, Issue 3, August vol. 16, Issue 3, July 2012, pp. 2-3, “Development • https://www.youtube.com/ 2017, p. 2, “Update on the Space Debris Sensor” of DRAGONS-An MMOD Impact Detection watch?v=O0i7-xqRF0s (launch recap accessed and pp. 3-6 “Benefits of a High LEO In-situ Sensor System”). Readers are further directed to 19 December 2017) Measurement Mission”; ODQN vol. 21, Issue 1, these online and social media resources: February 2017, p. 1, “Space Debris Sensor Waiting Reference for Launch” and pp. 9-10 “SDS is Readied for • https://www.nasa.gov/mission_ Hamilton, J., Liou, J.-C., Anz-Meador, P.D., Flight” photo feature; ODQN vol. 19, Issue 2, pages/station/research/news/sensor_to_ et al., “Development of the Space Debris Sensor,” April 2015, p. 11, “Space Debris Sensor (SDS) monitor_orbital_debris_outside_ISS 7th European Conference on Space Debris, testing in progress at NASA White Sands Test Darmstadt, Germany, published by ESA Space • @ (Twitter) Facility”; ODQN vol. 19, Issue 1, January 2015, ISS_Research Debris Office (April 2017). ♦ pp. 2-3, “DRAGONS to Fly on the ISS”; ODQN Figure 1. The SpaceX Dragon spacecraft successfully launched to the International Space Station Figure 2. The Dragon trunk following separation from the SpaceX Falcon 9 second at 10:36 a.m. EST Dec. 15, 2017, from Cape Canaveral Air Force Station in Florida. Credits: stage; clearly visible are the trunk payloads SDS at the 9 o’clock position and the Total NASA/Tony Gray and Sandra Joseph. Retrieved December 17 at https://www.nasa.gov/press- & Spectral solar Irradiance Sensor experiment at the 1 o’clock position. The Flight release/nasa-sends-new-research-to-space-station-aboard-spacex-resupply-mission . Releasable Attachment Mechanism station at the 5 o’clock position was fl wn empty for this flight Credit: NASA Figure 3. Having been installed robotically, in this artist's concept, the SDS resides at the ESA Columbus module’s EPF-SOX location. Credit: NASA 3 Orbital Debris Quarterly News PROJECT REVIEWS SEM Analysis Results of Returned ISS PMA-2 Cover J. HYDE, E. BERGER, D. LEAR, AND PMA-2 beta cloth of various diameters, shown in Hardware for MMOD Impacts,” 7th European E. CHRISTIANSEN solid lines for MEM-R2 and ORDEM 3.0 and with Conference on Space Debris, Darmstadt, In a previous Orbital Debris Quarterly News a dashed line for the MMOD total.
Recommended publications
  • APSCC Monthly E-Newsletter NOVEMBER 2017
    APSCC Monthly e-Newsletter NOVEMBER 2017 The Asia-Pacific Satellite Communications Council (APSCC) e-Newsletter is produced on a monthly basis as part of APSCC’s information services for members and professionals in the satellite industry. Subscribe to the APSCC monthly newsletter and be updated with the latest satellite industry news as well as APSCC activities! To renew your subscription, please visit www.apscc.or.kr/sub4_5.asp. To unsubscribe, send an email to [email protected] with a title “Unsubscribe.” News in this issue has been collected from October 1 to October 31. INSIDE APSCC The APSCC 2017 Conference & Exhibition Marks Another Great Success! The APSCC 2017 Satellite Conference & Exhibition successfully ended on 12 October 2017 in Tokyo after 3 days of in-depth conference sessions, state-of-the-art technology displayed exhibition, and diverse networking events with more than 400 delegates attending the event. At APSCC 2017, thought leaders covered major issues impacting the Asia-Pacific satellite industry, including market insight on the latest trends, new applications, and innovative technical solutions throughout the three-day roundtable discussions and presentation sessions. The APSCC 2018 Satellite Conference & Exhibition will be held on 9-11 October in Jakarta, Indonesia. The APSCC-ISU Youth Development Workshop The second APSCC-ISU Youth Development Workshop was successfully held concurrently with the APSCC 2017 event on October 12. The workshop provided a platform for the brightest up-and-coming engineering students and young professionals in Japan to connect with leading satellite and space industry experts and learn more about the opportunities in the sector.
    [Show full text]
  • 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.
    [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]
  • Space Biology Research and Biosensor Technologies: Past, Present, and Future †
    biosensors Perspective Space Biology Research and Biosensor Technologies: Past, Present, and Future † Ada Kanapskyte 1,2, Elizabeth M. Hawkins 1,3,4, Lauren C. Liddell 5,6, Shilpa R. Bhardwaj 5,7, Diana Gentry 5 and Sergio R. Santa Maria 5,8,* 1 Space Life Sciences Training Program, NASA Ames Research Center, Moffett Field, CA 94035, USA; [email protected] (A.K.); [email protected] (E.M.H.) 2 Biomedical Engineering Department, The Ohio State University, Columbus, OH 43210, USA 3 KBR Wyle, Moffett Field, CA 94035, USA 4 Mammoth Biosciences, Inc., South San Francisco, CA 94080, USA 5 NASA Ames Research Center, Moffett Field, CA 94035, USA; [email protected] (L.C.L.); [email protected] (S.R.B.); [email protected] (D.G.) 6 Logyx, LLC, Mountain View, CA 94043, USA 7 The Bionetics Corporation, Yorktown, VA 23693, USA 8 COSMIAC Research Institute, University of New Mexico, Albuquerque, NM 87131, USA * Correspondence: [email protected]; Tel.: +1-650-604-1411 † Presented at the 1st International Electronic Conference on Biosensors, 2–17 November 2020; Available online: https://iecb2020.sciforum.net/. Abstract: In light of future missions beyond low Earth orbit (LEO) and the potential establishment of bases on the Moon and Mars, the effects of the deep space environment on biology need to be examined in order to develop protective countermeasures. Although many biological experiments have been performed in space since the 1960s, most have occurred in LEO and for only short periods of time. These LEO missions have studied many biological phenomena in a variety of model organisms, and have utilized a broad range of technologies.
    [Show full text]
  • 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,
    [Show full text]
  • 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.
    [Show full text]
  • Spacex Rocket Data Satisfies Elementary Hohmann Transfer Formula E-Mail: [email protected] and [email protected]
    IOP Physics Education Phys. Educ. 55 P A P ER Phys. Educ. 55 (2020) 025011 (9pp) iopscience.org/ped 2020 SpaceX rocket data satisfies © 2020 IOP Publishing Ltd elementary Hohmann transfer PHEDA7 formula 025011 Michael J Ruiz and James Perkins M J Ruiz and J Perkins Department of Physics and Astronomy, University of North Carolina at Asheville, Asheville, NC 28804, United States of America SpaceX rocket data satisfies elementary Hohmann transfer formula E-mail: [email protected] and [email protected] Printed in the UK Abstract The private company SpaceX regularly launches satellites into geostationary PED orbits. SpaceX posts videos of these flights with telemetry data displaying the time from launch, altitude, and rocket speed in real time. In this paper 10.1088/1361-6552/ab5f4c this telemetry information is used to determine the velocity boost of the rocket as it leaves its circular parking orbit around the Earth to enter a Hohmann transfer orbit, an elliptical orbit on which the spacecraft reaches 1361-6552 a high altitude. A simple derivation is given for the Hohmann transfer velocity boost that introductory students can derive on their own with a little teacher guidance. They can then use the SpaceX telemetry data to verify the Published theoretical results, finding the discrepancy between observation and theory to be 3% or less. The students will love the rocket videos as the launches and 3 transfer burns are very exciting to watch. 2 Introduction Complex 39A at the NASA Kennedy Space Center in Cape Canaveral, Florida. This launch SpaceX is a company that ‘designs, manufactures and launches advanced rockets and spacecraft.
    [Show full text]
  • PRFP-11) & Interconnectivity Workshop 26-30 November 2019, Apia, SAMOA
    11th APT Policy and Regulation Forum for Pacific (PRFP-11) & Interconnectivity Workshop 26-30 November 2019, Apia, SAMOA Workshop Topic ENABLERS FOR A BETTER CONNECTED PACIFIC - New Satellite Technologies and Services (MSS, ESIM and LEOs) Dr Bob Horton Consultant Satellite Industry ENABLERS FOR A BETTER CONNECTED PACIFIC - New Satellite Technologies and Services (MSS and LEOs) CONTENTS • Examples of progress : MSS, ESIM – Inmarsat LEOs – OneWeb • Pacific Needs - understanding and participating in the regional/global environment - the Pacific : a “Collection of Islands” or an “Island Collective”? - opportunities overdue in APAC Inmarsat use of spectrum L band Ka band User links: 1626.5-1660.5 MHz ↑, 1525-1559 Feeder link ↑ : 27.5 – 30.0 GHz MHz↓ Feeder link↓ : 17.7 – 20.2 GHz Extended L-band: User link ↑ : 29.0 – 30.0 GHz User link↓ : 19.2 – 20.2 GHz User links: 1668-1675 MHz ↑, 1518 MHz-1525 MHz ↓ Used by Inmarsat Global Express satellites S band Used by Inmarsat-4 satellites and Alphasat Feeder link ↑ : 27.5 – 29.5 GHz Feeder link↓ : 17.7 – 19.7 GHz User link ↑ 1980-2010MHz Q/V band User link↓ : 2170-2200MHz C band 37.5-42.5 GHz ↓ Used by Europasat Feeder links for L-band satellites operate in 47.2-50.2 GHz + 50.4-51.4 GHz ↑ the bands 3550 – 3700 MHz and 6425 – - Planned for future satellites to free 6575 MHz through more than 20 Land Earth Stations up Ka-band for user terminals TT&C operated in standard C-band on most - Developmental payload on Alphasat Inmarsat satellites Inmarsat and Extended L-band Extended L-band will be available
    [Show full text]
  • The Annual Compendium of Commercial Space Transportation: 2017
    Federal Aviation Administration The Annual Compendium of Commercial Space Transportation: 2017 January 2017 Annual Compendium of Commercial Space Transportation: 2017 i Contents 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 (2017) Publication produced for FAA AST by The Tauri Group under contract. 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. ii Annual Compendium of Commercial Space Transportation: 2017 GENERAL CONTENTS Executive Summary 1 Introduction 5 Launch Vehicles 9 Launch and Reentry Sites 21 Payloads 35 2016 Launch Events 39 2017 Annual Commercial Space Transportation Forecast 45 Space Transportation Law and Policy 83 Appendices 89 Orbital Launch Vehicle Fact Sheets 100 iii Contents DETAILED CONTENTS EXECUTIVE SUMMARY .
    [Show full text]
  • 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.
    [Show full text]
  • Science & Technology
    2 INDEX 1. Space Technology ............................................... 6 1.38 Juno Spacecraft ......................................................... 20 1.1 Types of Orbits ............................................................ 6 1.39 OSIRIS-REx ............................................................... 20 1.2 Types of Satellites ........................................................ 7 1.40 Orion Spacecraft ........................................................ 21 1.3 Launch Vehicles .......................................................... 7 1.41 Voyager 1 & Voyager 2 ............................................. 21 1.42 Dawn Mission ............................................................ 21 Indian Missions ........................................................ 10 1.43 Europa Clipper Mission............................................. 22 1.4 PSLV C-44/Kalamsat ................................................ 10 1.44 Lucy and Psyche ........................................................ 22 1.5 PSLV C-43/HysIS ...................................................... 10 1.45 Magnetospheric Multiscale (MMS) Mission .............. 22 1.6 HySIS ......................................................................... 11 1.46 CubeSat...................................................................... 23 1.7 PSLV C-42................................................................. 11 1.47 NICER ....................................................................... 23 1.8 PSLV C-41/IRNSS-1I................................................
    [Show full text]
  • Koreasat-5A Mission
    Koreasat-5A Mission Mission Overview SpaceX’s Falcon 9 rocket will deliver Koreasat-5A, a commercial communications satellite, to a Geostationary Transfer Orbit (GTO). SpaceX is targeting launch of Koreasat-5A from Launch Complex 39A (LC-39A) at NASA’s Kennedy Space Center, Florida. The primary launch window opens on Monday, October 30 at 3:34 p.m. EDT, or 19:34 UTC and closes at 5:58 p.m. EDT, or 21:58 UTC. A backup launch window opens on Tuesday, October 31 at 3:34 p.m. EDT, or 19:34 UTC and closes at 5:58 p.m. EDT, or 21:58 UTC. The satellite will be deployed approximately 36 minutes after liftoff. Following stage separation, Falcon 9’s first stage will attempt a landing on the “Of Course I Still Love You” droneship, which will be stationed in the Atlantic Ocean. Official SpaceX Koreasat-5A mission patch Payload Koreasat-5A is a communications satellite operated by KT SAT, South Korea’s sole satellite service provider. Manufactured by Thales Alenia Space and located at 113°E, Koreasat-5A will provide Direct-to-Home (DTH) broadcast, broadband, and backhaul services with its Ku-Band capacity. Koreasat-5A provides KT SAT with 12 Ku-band transponders of 36MHz, and 24 Ku-band transponders of 54MHz. As a replacement for Koreasat-5, Koreasat-5A will expand KT SAT’s coverage across Asia and the Middle East. Unlike other satellites in the Koreasat fleet, Koreasat-5A will provide maritime coverage of the Persian Gulf, Indian Ocean, South China Sea, and East China Sea.
    [Show full text]