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General Assembly Distr.: General 29 January 2001
United Nations A/AC.105/751/Add.1 General Assembly Distr.: General 29 January 2001 Original: English Committee on the Peaceful Uses of Outer Space National research on space debris, safety of space objects with nuclear power sources on board and problems of their collisions with space debris Note by the Secretariat* Addendum Contents Chapter Paragraphs Page I. Introduction........................................................... 1-2 2 Replies received from Member States and international organizations .................... 2 United States of America ......................................................... 2 European Space Agency.......................................................... 7 __________________ * The present document contains replies received from Member States and international organizations between 25 November 2000 and 25 January 2001. V.01-80520 (E) 020201 050201 A/AC.105/751/Add.1 I. Introduction 1. At its forty-third session, the Committee on the Peaceful Uses of Outer Space agreed that Member States should continue to be invited to report to the Secretary- General on a regular basis with regard to national and international research concerning the safety of space objects with nuclear power sources, that further studies should be conducted on the issue of collision of orbiting space objects with nuclear power sources on board with space debris and that the Committee’s Scientific and Technical Subcommittee should be kept informed of the results of such studies.1 The Committee also took note of the agreement of the Subcommittee that national research on space debris should continue and that Member States and international organizations should make available to all interested parties the results of that research, including information on practices adopted that had proved effective in minimizing the creation of space debris (A/AC.105/736, para. -
University of Iowa Instruments in Space
University of Iowa Instruments in Space A-D13-089-5 Wind Van Allen Probes Cluster Mercury Earth Venus Mars Express HaloSat MMS Geotail Mars Voyager 2 Neptune Uranus Juno Pluto Jupiter Saturn Voyager 1 Spaceflight instruments designed and built at the University of Iowa in the Department of Physics & Astronomy (1958-2019) Explorer 1 1958 Feb. 1 OGO 4 1967 July 28 Juno * 2011 Aug. 5 Launch Date Launch Date Launch Date Spacecraft Spacecraft Spacecraft Explorer 3 (U1T9)58 Mar. 26 Injun 5 1(U9T68) Aug. 8 (UT) ExpEloxrpelro r1e r 4 1915985 8F eJbu.l y1 26 OEGxOpl o4rer 41 (IMP-5) 19697 Juunlye 2 281 Juno * 2011 Aug. 5 Explorer 2 (launch failure) 1958 Mar. 5 OGO 5 1968 Mar. 4 Van Allen Probe A * 2012 Aug. 30 ExpPloiorenre 3er 1 1915985 8M Oarc. t2. 611 InEjuxnp lo5rer 45 (SSS) 197618 NAouvg.. 186 Van Allen Probe B * 2012 Aug. 30 ExpPloiorenre 4er 2 1915985 8Ju Nlyo 2v.6 8 EUxpKlo 4r e(rA 4ri1el -(4IM) P-5) 197619 DJuenc.e 1 211 Magnetospheric Multiscale Mission / 1 * 2015 Mar. 12 ExpPloiorenre 5e r 3 (launch failure) 1915985 8A uDge.c 2. 46 EPxpiolonreeerr 4130 (IMP- 6) 19721 Maarr.. 313 HMEaRgCnIe CtousbpeShaetr i(cF oMxu-1ltDis scaatelell itMe)i ssion / 2 * 2021081 J5a nM. a1r2. 12 PionPeioenr e1er 4 1915985 9O cMt.a 1r.1 3 EExpxlpolorerer r4 457 ( S(IMSSP)-7) 19721 SNeopvt.. 1263 HMaalogSnaett oCsupbhee Sriact eMlluitlet i*scale Mission / 3 * 2021081 M5a My a2r1. 12 Pioneer 2 1958 Nov. 8 UK 4 (Ariel-4) 1971 Dec. 11 Magnetospheric Multiscale Mission / 4 * 2015 Mar. -
Information Summaries
TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
This Boeing Team's Skills at Producing Delta IV Rocket Fairings Helped
t’s usually the tail end of the rocket that gets all the early atten- other work. But they’d jump at the chance to work together again. tion, providing an impressive fiery display as the spacecraft is Their story is one of challenges and solutions. And they attribute hurled into orbit. But mission success also depends on what’s their success to Lean+ practices and good old-fashioned teamwork. Ion top of the rocket: a piece of metal called the payload fairing “The team took it upon themselves to make an excellent that protects the rocket’s cargo during the sometimes brutal ride product,” said program manager Thomas Fung. “We had parts to orbital speed. issues and tool problems, but the guys really stepped up and took “There’s no room for error,” said Tracy Allen, Boeing’s manu- pride and worked through the issues.” facturing production manager for a Huntington Beach, Calif., team The aluminum fairing team went through a major transition that made fairings for the Delta IV. The fairing not only protects the when Boeing merged its Delta Program with Lockheed Martin’s payload from launch to orbit but also must jettison properly for Atlas Program to form United Launch Alliance in 2006. deployment of the satellite or spacecraft. “There were a lot of process changes in the transition phase Allen and his colleagues built the 65-foot-long (20-meter-long) because we were working with a new company,” Fung said. “We aluminum isogrid fairings for the Delta IV heavy-lift launch vehicle. had part shortages because of vendor issues, and that caused The design was based on 41 similar fairings Boeing made for the an impact to the schedule. -
The SKYLON Spaceplane
The SKYLON Spaceplane Borg K.⇤ and Matula E.⇤ University of Colorado, Boulder, CO, 80309, USA This report outlines the major technical aspects of the SKYLON spaceplane as a final project for the ASEN 5053 class. The SKYLON spaceplane is designed as a single stage to orbit vehicle capable of lifting 15 mT to LEO from a 5.5 km runway and returning to land at the same location. It is powered by a unique engine design that combines an air- breathing and rocket mode into a single engine. This is achieved through the use of a novel lightweight heat exchanger that has been demonstrated on a reduced scale. The program has received funding from the UK government and ESA to build a full scale prototype of the engine as it’s next step. The project is technically feasible but will need to overcome some manufacturing issues and high start-up costs. This report is not intended for publication or commercial use. Nomenclature SSTO Single Stage To Orbit REL Reaction Engines Ltd UK United Kingdom LEO Low Earth Orbit SABRE Synergetic Air-Breathing Rocket Engine SOMA SKYLON Orbital Maneuvering Assembly HOTOL Horizontal Take-O↵and Landing NASP National Aerospace Program GT OW Gross Take-O↵Weight MECO Main Engine Cut-O↵ LACE Liquid Air Cooled Engine RCS Reaction Control System MLI Multi-Layer Insulation mT Tonne I. Introduction The SKYLON spaceplane is a single stage to orbit concept vehicle being developed by Reaction Engines Ltd in the United Kingdom. It is designed to take o↵and land on a runway delivering 15 mT of payload into LEO, in the current D-1 configuration. -
UHD with Asiasat
UHD with AsiaSat Alan WONG Manager, Sales Solutions 23 Jun 2016 AsiaSat Proprietary & Confidential AsiaSat Proprietary & Confidential Contents • Brief Introduction of AsiaSat • Hands-on Satellite Transmission • Our Engagement with UHD • How we see UHD? • AsiaSat UHD Platform • Next Step AsiaSat Proprietary & Confidential UHD with AsiaSat 2 Brief Introduction of AsiaSat Our Background Our Satellite Fleet Our Facilities Our People AsiaSat Proprietary & Confidential AsiaSat Corporate Video AsiaSat Proprietary & Confidential UHD with AsiaSat 4 Our Background Head-quartered in Hong Kong Established in 1988 Listing in Hong Kong Stock Exchange Regional Satellite Operator • Asia’s leading satellite operator, aiming to provide highest quality satellite communications services in the region Coverage • Across 50 countries in Asia-Pacific • Reaching 2/3 of world's population Customer Profile • International and Regional TV Broadcasters • Telecommunications Service Providers • News Agencies • Corporations and Governments AsiaSat Proprietary & Confidential UHD with AsiaSat 5 Our Satellite Fleet C-band Ku-band For more details of our satellite fleet, please visit our web site (http://www.asiasat.com/technology/satellite-fleet). AsiaSat Proprietary & Confidential UHD with AsiaSat 6 Our Earth Stations Tai Po Earth Station Stanley Earth Station For more details of our facilities, please visit our web site (http://www.asiasat.com/aboutus/facilities). AsiaSat Proprietary & Confidential UHD with AsiaSat 7 Tai Po Earth Station AsiaSat Tai Po Earth Station is Antennas Services • 1x 1.3m (C) • Uplink Service located at the Tai Po Industrial • 2x 9.0m (C) • Downlink Service Estate in the New Territories, • 3x 7.3m (C) • Occasional Service Hong Kong. • 2x 6.3m (C) • Conditional Access • 1x 6.1m (C) Service • 4x 7.3m (Ku) • Compression Service • 2x 6.3m (Ku) • Playout Service The Station is a two level building • 1x 4.9m (Ku) • Monitoring Service of 5,551 sq.m. -
GB-ASTRA 3B-Comsatbw-21Mai V
A BOOST FOR SPACE COMMUNICATIONS SATELLITES For its first launch of the year, Arianespace will orbit two communications satellites: ASTRA 3B for the Luxembourg-based operator SES ASTRA, and COMSATBw-2 for Astrium as part of a contract with the German Ministry of Defense. The choice of Arianespace by leading space communications operators and manufacturers is clear international recognition of the company’s excellence in launch services. Because of its reliability and availability, the Arianespace launch system continues to set the global standard. Ariane 5 is the only commercial satellite launcher now on the market capable of simultaneously launching two payloads. Over the last two decades, Arianespace and SES have developed an exceptional relationship. ASTRA 3B will be the 33rd satellite from the SES group (Euronext Paris and Luxembourg Bourse: SESG) to have chosen the European launcher. SES ASTRA operates the leading direct-to-home TV broadcast system in Europe, serving more than 125 million households via DTH and cable networks. ASTRA 3B was built by Astrium using a Eurostar E 3000 platform, and will weigh approximately 5,500 kg at launch. Fitted with 60 active Ku-band transponders and four Ka-band transponders, ASTRA 3B will be positioned at 23.5 degrees East. It will deliver high-power broadcast services across all of Europe, and offers a design life of 15 years. Astrium chose Arianespace for the launch of two military communications satellites, COMSATBw-1 and COMSATBw-2, as part of a satellite communications system supplied to the German Ministry of Defense. The first satellite in this family, COMSATBw-1, was launched by Arianespace in October 2009. -
(50000) Quaoar, See Quaoar (90377) Sedna, See Sedna 1992 QB1 267
Index (50000) Quaoar, see Quaoar Apollo Mission Science Reports 114 (90377) Sedna, see Sedna Apollo samples 114, 115, 122, 1992 QB1 267, 268 ap-value, 3-hour, conversion from Kp 10 1996 TL66 268 arcade, post-eruptive 24–26 1998 WW31 274 Archimedian spiral 11 2000 CR105 269 Arecibo observatory 63 2000 OO67 277 Ariel, carbon dioxide ice 256–257 2003 EL61 270, 271, 273, 274, 275, 286, astrometric detection, of extrasolar planets – mass 273 190 – satellites 273 Atlas 230, 242, 244 – water ice 273 Bartels, Julius 4, 8 2003 UB313 269, 270, 271–272, 274, 286 – methane 271–272 Becquerel, Antoine Henry 3 – orbital parameters 271 Biermann, Ludwig 5 – satellite 272 biomass, from chemolithoautotrophs, on Earth 169 – spectroscopic studies 271 –, – on Mars 169 2005 FY 269, 270, 272–273, 286 9 bombardment, late heavy 68, 70, 71, 77, 78 – atmosphere 273 Borealis basin 68, 71, 72 – methane 272–273 ‘Brown Dwarf Desert’ 181, 188 – orbital parameters 272 brown dwarfs, deuterium-burning limit 181 51 Pegasi b 179, 185 – formation 181 Alfvén, Hannes 11 Callisto 197, 198, 199, 200, 204, 205, 206, ALH84001 (martian meteorite) 160 207, 211, 213 Amalthea 198, 199, 200, 204–205, 206, 207 – accretion 206, 207 – bright crater 199 – compared with Ganymede 204, 207 – density 205 – composition 204 – discovery by Barnard 205 – geology 213 – discovery of icy nature 200 – ice thickness 204 – evidence for icy composition 205 – internal structure 197, 198, 204 – internal structure 198 – multi-ringed impact basins 205, 211 – orbit 205 – partial differentiation 200, 204, 206, -
Echostar DBS Corporation
Table of Contents UNITED STATES SECURITIES AND EXCHANGE COMMISSION Washington, D.C. 20549 Form 10-Q (Mark One) [X] QUARTERLY REPORT PURSUANT TO SECTION 13 OR 15(d) OF THE SECURITIES EXCHANGE ACT OF 1934 FOR THE QUARTERLY PERIOD ENDED JUNE 30, 2004 OR [ ] TRANSITION REPORT PURSUANT TO SECTION 13 OR 15(d) OF THE SECURITIES EXCHANGE ACT OF 1934 For the transition period from to . Commission File Number 333-31929 EchoStar DBS Corporation (Exact name of registrant as specified in its charter) Colorado 84-1328967 (State or other jurisdiction of incorporation or organization) (I.R.S. Employer Identification No.) 9601 South Meridian Boulevard Englewood, Colorado 80112 (Address of principal executive offices) (Zip code) (303) 723-1000 (Registrant’s telephone number, including area code) Not Applicable (Former name, former address and former fiscal year, if changed since last report) Indicate by check mark whether the registrant (1) has filed all reports required to be filed by Section 13 or 15(d) of the Securities Exchange Act of 1934 during the preceding 12 months (or for such shorter period that the registrant was required to file such reports), and (2) has been subject to such filing requirements for the past 90 days. Yes [X] No [ ] Indicate by check mark whether the registrant is an accelerated filer (as defined by Rule 12b-2 of the Exchange Act). Yes [ ] No [X] As of July 30, 2004, the Registrant’s outstanding common stock consisted of 1,015 shares of Common Stock, $0.01 par value. The Registrant meets the conditions set forth in General Instruction (H)(1)(a) and (b) of Form 10-Q and is therefore filing this Form 10-Q with the reduced disclosure format. -
Small Satellite Launchers
SMALL SATELLITE LAUNCHERS NewSpace Index 2020/04/20 Current status and time from development start to the first successful or planned orbital launch NEWSPACE.IM Northrop Grumman Pegasus 1990 Scorpius Space Launch Demi-Sprite ? Makeyev OKB Shtil 1998 Interorbital Systems NEPTUNE N1 ? SpaceX Falcon 1e 2008 Interstellar Technologies Zero 2021 MT Aerospace MTA, WARR, Daneo ? Rocket Lab Electron 2017 Nammo North Star 2020 CTA VLM 2020 Acrux Montenegro ? Frontier Astronautics ? ? Earth to Sky ? 2021 Zero 2 Infinity Bloostar ? CASIC / ExPace Kuaizhou-1A (Fei Tian 1) 2017 SpaceLS Prometheus-1 ? MISHAAL Aerospace M-OV ? CONAE Tronador II 2020 TLON Space Aventura I ? Rocketcrafters Intrepid-1 2020 ARCA Space Haas 2CA ? Aerojet Rocketdyne SPARK / Super Strypi 2015 Generation Orbit GoLauncher 2 ? PLD Space Miura 5 (Arion 2) 2021 Swiss Space Systems SOAR 2018 Heliaq ALV-2 ? Gilmour Space Eris-S 2021 Roketsan UFS 2023 Independence-X DNLV 2021 Beyond Earth ? ? Bagaveev Corporation Bagaveev ? Open Space Orbital Neutrino I ? LIA Aerospace Procyon 2026 JAXA SS-520-4 2017 Swedish Space Corporation Rainbow 2021 SpinLaunch ? 2022 Pipeline2Space ? ? Perigee Blue Whale 2020 Link Space New Line 1 2021 Lin Industrial Taymyr-1A ? Leaf Space Primo ? Firefly 2020 Exos Aerospace Jaguar ? Cubecab Cab-3A 2022 Celestia Aerospace Space Arrow CM ? bluShift Aerospace Red Dwarf 2022 Black Arrow Black Arrow 2 ? Tranquility Aerospace Devon Two ? Masterra Space MINSAT-2000 2021 LEO Launcher & Logistics ? ? ISRO SSLV (PSLV Light) 2020 Wagner Industries Konshu ? VSAT ? ? VALT -
NASA Expendable Launch Services Current Use of EELV
NASA Expendable Launch Services Current Use of EELV Lynn F. H. Cline Deputy Associate Administrator for Space Operations National Aeronautics and Space Administration June 17, 2009 Overview • NASA’s expendable launch vehicles are run by the Launch Services Program (LSP) consolidated at Kennedy Space Center in 1998 – LSP provides acquisition, technical management, mission integration and launch management • NASA utilizes a mixed fleet of vehicles (small, medium & intermediate) with varying levels of performance used to support a mix of mission sizes – Mainly for Science Mission Directorate payloads, but other NASA Directorates and other government agencies also use NASA launch services – Launches conducted from multiple ranges, including RTS, WFF, Kodiak • Vehicles are selected from the NASA Launch Services Contract (NLS) – Through competition based on mass, orbit, class of payload, and best value – Current NLS contract expires in 2010, RFP released to extend the contract • Most recent contract action purchased four intermediate class missions – TDRS – K & L, RBSP and MMS • Important issues – Loss of Medium Class launch service provider, which has been 50% of NASA missions historically – Compressed manifest – Possibility that NASA incurs a portion of the intermediate class infrastructure costs post 2010 NASA Launch Services Manifest FPB Approved 3/25/09 2009 2010 2011 2012 2013 2014 2015 2016 Release 6/03/09 Rev. 1 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Q1 Q2 Q3 Q4 Small Class (SC) NuSTAR (P-XL) -
Grin,Yaue T: M, 2
4 w .. -. I 1 . National Aeronautics and STace Administration Goddard Space Flight Center C ont r ac t No NAS -5 -f 7 60 THE OUTERMOST BELT OF CFLARGED PARTICLES _- .- - by K. I, Grin,yaue t: M, 2. I~alOkhlOV cussa 3 GPO PRICE $ CFSTI PRICE(S) $ 17 NOVEbI3ER 1965 Hard copy (HC) .J d-0 Microfiche (M F) ,J3’ ff 853 July 85 Issl. kosniicheskogo prostrznstva by K. N. Gringaua Trudy Vsesoyuzrloy koneferentsii & M. z. Khokhlov po kosaiches?%inlucham, 467 - 482 Noscon, June 1965. This report deals with the result of the study of a eone of char- ged pxticles with comparatively low ener-ies (from -100 ev to 10 - 4Okev), situated beyond the outer rzdiation belt (including the new data obtained on Ilectron-2 and Zond-2). 'The cutkors review, first of all, an2 in chronolo~icalorder, the space probes on which data on soft electrons 'and protons were obtained beyond the rsdistion belts. A brief review is given of soae examples of regis- tration of soft electrons at high geominetic latitudes by Mars-1 and Elec- tron-2. It is shown that here, BS in other space probes, the zones of soft electron flwcys are gartly overlap7inr with the zones of trapped radiation. The spatial distributio;: of fluxcs of soft electrons is sixdied in liqht of data oStziined fro.1 various sFnce probes, such as Lunik-1, Explorer-12, Explorer-18, for the daytime rerion along the map-etosphere boundary &om the sumy side. The night re-ion of fluxes is exmined fron data provided by Lunik-2, 7xpiorer-12, Z~nd-2~~ni the results of various latest works with reKarr! to the relationshi- of that distribution with the structure of tire marnetic field are exCmined and cornpcved.