Quarterly Launch Report
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Ariane-5 Completes Flawless Third Test Flight
r bulletin 96 — november 1998 Ariane-5 Completes Flawless Third Test Flight A launch-readiness review conducted on Friday engine shut down and Maqsat-3 was 16 and Monday 19 October had given the go- successfully injected into GTO. The orbital ahead for the final countdown for a launch just parameters at that point were: two days later within a 90-minute launch Perigee: 1027 km, compared with the window between 13:00 to 14:30 Kourou time. 1028 ± 3 km predicted The launcher’s roll-out from the Final Assembly Apogee: 35 863 km, compared with the Building to the Launch Zone was therefore 35 898 ± 200 km predicted scheduled for Tuesday 20 October at 09:30 Inclination: 6.999 deg, compared with the Kourou time. 6.998 ± 0.05 deg predicted. On 21 October, Europe reconfirmed its lead in providing space Speaking in Kourou immediately after the flight, transportation systems for the 21st Century. Ariane-5, on its third Fredrik Engström, ESA’s Director of Launchers qualification flight, left no doubts as to its ability to deliver payloads and the Ariane-503 Flight Director, confirmed reliably and accurately to Geostationary Transfer Orbit (GTO). The new that: “The third Ariane-5 flight has been a heavy-lift launcher lifted off in glorious sunshine from the Guiana complete success. It qualifies Europe’s new Space Centre, Europe’s spaceport in Kourou, French Guiana, at heavy-lift launcher and vindicates the 13:37:21 local time (16:37:21 UT). technological options chosen by the European Space Agency.” This third Ariane-5 test flight was intended ESA’s Director -
Leviathan Leviathan
Leviathan™ st Low Cost Heavy Lift for the 21 Century™ Approved For Public Distribution - Copyright © 2011, DIRECT - All Rights Reserved Leviathan™ st Low Cost Heavy Lift for the 21 Century™ ™ The centerpiece of DIRECT ’s new fleet of space systems, Leviathan™, is a brand-new breed of low cost commercial heavy lift launch vehicle. It is specifically designed to provide unrivaled performance at a price that will finally enable affordable industrial access to space. Leviathan™ With a Payload Fairing diameter of 13.80 meters and a payload capacity over 140 metric tons, Leviathan™ is significantly larger than any other launch vehicle in history, including the Saturn-V rocket that once took astronauts to the moon. Nation / Vehicle Mission Reliability Launch Cost† LEO Payload† Cost / kg to LEO Space Shuttle 130 of 132 (98.48%) $850 million 24,400 kg $34,836 Delta-IV Heavy 13 of 14 (92.86%) $265 million 23,040 kg $11,502 Atlas-V 552 22 of 23 (95.65%) $190 million 20,050 kg $9,476 Ariane-V ES 51.55 (92.73%) $120 million 21,000 kg $5,714 Falcon-9 <Insufficient Data> $56 million 10,450 kg $5,359 Long March 2E 112 of 122 (91.80%) $55 million 14,100 kg $3,901 Proton-M 294 of 335 (87.76%) $80 million 21,000 kg $3,810 Leviathan™ 98.00% * $60 million * 140,000 kg * $429 * * Initial Estimates based on 6 flights per year † Based on publicly available information Leviathan™ is designed to be fully reusable (except the payload fairings) with a minimum of inspections and maintenance between flights. -
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 -
Secretariat GENERAL ST/SG/SER.E/320 23 May 1997 ENGLISH ORIGINAL: RUSSIAN
UNITED NATIONS ST Distr. Secretariat GENERAL ST/SG/SER.E/320 23 May 1997 ENGLISH ORIGINAL: RUSSIAN COMMITTEE ON THE PEACEFUL USES OF OUTER SPACE INFORMATION FURNISHED IN CONFORMITY WITH THE CONVENTION ON REGISTRATION OF OBJECTS LAUNCHED INTO OUTER SPACE Note verbale dated 15 April 1997 from the Permanent Mission of the Russian Federation to the United Nations (Vienna) addressed to the Secretary-General The Permanent Mission of the Russian Federation to the United Nations (Vienna) presents its compliments to the Secretary-General of the United Nations and, in accordance with article IV of the Convention on Registration of Objects Launched into Outer Space,* has the honour to transmit information concerning space objects launched by the Russian Federation from April to December 1996 and conce rning Russian space objects which ceased to exist within those same periods of time and are no longer in Earth orbit (see annex). *General Assembly resolution 3235 (XXIX), annex, of 12 November 1974. V.97-23994T ST/SG/SER.E/320 Page 2 ST/SG/SER.E/320 Page 3 ST/SG/SER.E/320 Page 4 ST/SG/SER.E/320 Page 5 ST/SG/SER.E/320 Page 6 ST/SG/SER.E/320 Page 7 ST/SG/SER.E/320 Page 8 ST/SG/SER.E/320 Page 9 Annex* REGISTRATION DATA ON SPACE OBJECTS LAUNCHED BY THE RUSSIAN FEDERATION IN APRIL 1996 1. In April 1996, the Russian Federation launched the following space objects: Basic orbit characteristics Date of Apogee Perigee Inclination Period No. Name of space object launching (km) (km) (degrees) (minutes) General purpose of space object 2985 Priroda 23 April 347 220 51.6 89.9 The Priroda module is intended for the per- (launched by a Proton carrier rocket formance of research and experiments by the crew from the Baikonur launch site) of the Mir orbital station, partly under the programme of cooperation between the Russian Federation and the United States of America 2986 Cosmos-2332 24 April 1 585 304 83 104 The space object is intended for assignments on (launched by a Cosmos carrier rocket behalf of the Ministry of Defence of the Russian from the Plesetsk launch site) Federation 2. -
US National Security and Military/Commercial
COMMERCIAL SPACE INSURANCE VOLUME II: Chapter 8/Summary he space insurance aspect of the Intelsat 708 launch failure focuses on the exchange of controlled technical information within the insurance community. Insurance underwriters and reinsurers for the Apstar 1A satellite program — the next scheduled T satellite to be launched on the Long March 3B after the Intelsat 708 failure — were concerned about the reliability of the Long March rocket, and the fate of future launch insurance programs in the PRC. Immediately after the Intelsat 708 launch failure, space insurance under- writers for the Apstar 1A insurance program pressured the PRC to create an international and Independent Review Committee (IRC). These underwriters and reinsurers insisted on this arrangement to ensure that an adequate assessment of the risks of future Long March rocket launches was made. Representatives from J & H Marsh & McLennan, an international space insurance brokerage firm, were adamant about obtaining a report from the Independent Review Committee for the benefit of the reinsurers of the Apstar 1A satellite insurance program. Members of the space insurance community were invit- ed to attend a meeting on April 15 and 16, 1996, in the PRC. The purpose of the meet- ing was to build confidence in the Long March rocket, and to discuss the status of the Apstar 1A insurance program. The space insurance acquisition and underwriting process includes the dis- semination of technical information, the consideration of market conditions, capac- ity, and participants, and the involvement of insurance brokers, underwriters, and rein- surers. This chapter identifies several issues relating to procedures for the disclosure and handling of sensitive information by the insurance community. -
Commercial Space Transportation Developments and Concepts: Vehicles, Technologies and Spaceports
Commercial Space Transportation 2006 Commercial Space Transportation Developments and Concepts: Vehicles, Technologies and Spaceports January 2006 HQ003606.INDD 2006 U.S. Commercial Space Transportation Developments and Concepts About FAA/AST About the 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 49 United States Code, Subtitle IX, Chapter 701 (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 encour- age, facilitate, and promote commercial space launches and reentries. Additional information concerning commercial space transportation can be found on FAA/AST’s web site at http://ast.faa.gov. Federal Aviation Administration Office of Commercial Space Transportation i About FAA/AST 2006 U.S. Commercial Space Transportation Developments and Concepts 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 Federal Aviation Administration Office of Commercial Space Transportation 2006 U.S. Commercial Space Transportation Developments and Concepts Contents Table of Contents Introduction . .1 Significant 2005 Events . .4 Space Competitions . .6 Expendable Launch Vehicles . .9 Current Expendable Launch Vehicle Systems . .9 Atlas 5 - Lockheed Martin Corporation . -
AMC-14 MO Final.Qxp 2/29/2008 1:15 PM Page 1
AMC-14 MO final.qxp 2/29/2008 1:15 PM Page 1 THE VEHICLE THE SATELLITE PROTON HISTORY PROTON www.ilslaunch.com Lead designer was Vladimir Chelomei, DESCRIPTION who designed it with the intention of creating a powerful rocket for both TOTAL HEIGHT military payloads and as a high- 56.2 m (184 ft) performance ICBM. The program GROSS LIFTOFF was changed, and the rocket WEIGHT was developed exclusively for 691,272 kg launching spacecraft. (1,523,565 lbm) First named UR-500, but PROPELLANT UDMH and N O adopted the name 2 4 “Proton,” which also was INITIAL LAUNCH the name of the first July 16, 1965 three payloads Proton-1 Spacecraft launched. PAYLOAD FAIRINGS Proton launched Russian There are multiple payload fair- ing designs presently qualified for interplanetary missions to flight, including standard commer- the Moon, Venus, Mars, and cial payload fairings developed specif- Halley’s Comet. ically to meet the needs of our Western customers. Proton launched the Salyut space stations, the Mir BREEZE M UPPER STAGE SATELLITE OPERATOR core segment and both The Breeze M is powered by one pump-fed gim- SES AMERICOM baled main engine that develops thrust of 19.6 kN the Zarya and Zvezda www.ses-americom.com (4,400 lbf). The Breeze M is composed of a central core modules for today’s and a jettisonable additional propellant tank. Inert mass of the SATELLITE MANUFACTURER International Space stage at liftoff is approximately 2,370 kg (5,225 lbm). The quan- Lockheed Martin Commercial Space Systems Station. tity of propellant carried is dependent on specific mission require- www.lmcommercialspace.com ments and is varied to maximize mission performance. -
L AUNCH SYSTEMS Databk7 Collected.Book Page 18 Monday, September 14, 2009 2:53 PM Databk7 Collected.Book Page 19 Monday, September 14, 2009 2:53 PM
databk7_collected.book Page 17 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS databk7_collected.book Page 18 Monday, September 14, 2009 2:53 PM databk7_collected.book Page 19 Monday, September 14, 2009 2:53 PM CHAPTER TWO L AUNCH SYSTEMS Introduction Launch systems provide access to space, necessary for the majority of NASA’s activities. During the decade from 1989–1998, NASA used two types of launch systems, one consisting of several families of expendable launch vehicles (ELV) and the second consisting of the world’s only partially reusable launch system—the Space Shuttle. A significant challenge NASA faced during the decade was the development of technologies needed to design and implement a new reusable launch system that would prove less expensive than the Shuttle. Although some attempts seemed promising, none succeeded. This chapter addresses most subjects relating to access to space and space transportation. It discusses and describes ELVs, the Space Shuttle in its launch vehicle function, and NASA’s attempts to develop new launch systems. Tables relating to each launch vehicle’s characteristics are included. The other functions of the Space Shuttle—as a scientific laboratory, staging area for repair missions, and a prime element of the Space Station program—are discussed in the next chapter, Human Spaceflight. This chapter also provides a brief review of launch systems in the past decade, an overview of policy relating to launch systems, a summary of the management of NASA’s launch systems programs, and tables of funding data. The Last Decade Reviewed (1979–1988) From 1979 through 1988, NASA used families of ELVs that had seen service during the previous decade. -
From Strength to Strength Worldreginfo - 24C738cf-4419-4596-B904-D98a652df72b 2011 SES Astra and SES World Skies Become SES
SES Annual report 2013 Annual Annual report 2013 From strength to strength WorldReginfo - 24c738cf-4419-4596-b904-d98a652df72b 2011 SES Astra and SES World Skies become SES 2010 2009 3rd orbital position Investment in O3b Networks over Europe 2008 2006 SES combines Americom & Coverage of 99% of New Skies into SES World Skies the world’s population 2005 2004 SES acquires New Skies Satellites Launch of HDTV 2001 Acquisition of GE Americom 1999 First Ka-Band payload in orbit 1998 Astra reaches 70m households in Europe Second orbital slot: 28.2° East 1996 SES lists on Luxembourg Stock Exchange First SES launch on Proton: ASTRA 1F Digital TV launch 1995 ASTRA 1E launch 1994 ASTRA 1D launch 1993 ASTRA 1C launch 1991 ASTRA 1B launch 1990 World’s first satellite co-location Astra reach: 16.6 million households in Europe 1989 Start of operations @ 19.2° East 1988 ASTRA 1A launches on board Ariane 4 1st satellite optimised for DTH 1987 Satellite control facility (SCF) operational 1985 SES establishes in Luxembourg Europe’s first private satellite operator WorldReginfo - 24c738cf-4419-4596-b904-d98a652df72b 2012 First emergency.lu deployment SES unveils Sat>IP 2013 SES reach: 291 million TV households worldwide SES maiden launch with SpaceX More than 6,200 TV channels 1,800 in HD 2010 First Ultra HD demo channel in HEVC 3rd orbital position over Europe 25 years in space With the very first SES satellite, ASTRA 1A, launched on December 11 1988, SES celebrated 25 years in space in 2013. Since then, the company has grown from a single satellite/one product/one-market business (direct-to-home satellite television in Europe) into a truly global operation. -
Annual Report 2018
RAPPORT D'ACTIVITÉ ANNUAL REPORT 2018 Mission InSight-SEIS La France sur Mars InSight-SEIS mission France on Mars 4 ÉDITORIAL FOREWORD Avec ses coopérations sur tous les continents, le CNES est une référence incontournable 2018 a été Nous sommes aussi partis vers la steppe du Kazakhstan, au retour sur particulièrement Mercure avec le lancement de la sonde Terre de Thomas Pesquet, il avait eu BepiColombo le 26 octobre, sans oublier l’intuition de ce projet. réussie pour le CNES que le 3 octobre, l’atterrisseur Mascot Nous avons donc immédiatement s’était posé sur l’astéroïde Ryugu. avec des succès partagé cette idée avec nos Côté observation, nous avons bien partenaires du monde entier et le SCO majeurs : lancement terminé l’année avec le lancement des satellites CFOSat, de MetOp-C et auparavant, nous a été lancé par Frédérique Vidal, le MetOp-C, CSO-1 avions lancé avec la Chine, CFOSat 11 décembre 2017 lors de la première pour l’étude du vent et des vagues. édition du One Planet Summit et et de la sonde présenté à de nombreux Chefs d’État interplanétaire En matière de télécommunications, à New-York, le 26 septembre 2018. BepiColombo, l’année a aussi été intense avec le La signature de l’acte fondateur du succès planétaire de la constellation SCO sera l’un des temps forts de 2019 naissance du SCO Galileo et avec la décision de et rappellera que les satellites sont (le Space Climate développer le satellite Konnect pour incontournables dans la lutte contre Observatory), création que la totalité des habitants de le changement climatique. -
Table of Contents
VOLUME II: CONTENTS ALL-VOLUME OVERVIEW . .i CHAPTER 5 Satellite Launches in the PRC: Hughes CHAPTER SUMMARY . 2 OPTUS B2, APSTAR 2 LAUNCH FAILURES: PRC GAINS SENSITIVE KNOWLEDGE FROM HUGHES INVESTIGATIONS . 6 THE PROHIBITION AGAINST TECHNOLOGY TRANSFER IN FOREIGN LAUNCHES . 8 International Traffic in Arms Regulations and the U.S. Munitions List . 8 Department of Defense Monitoring Role . 9 OPTUS B2 . .10 The Optus B2 Licenses . 10 The Optus B2 Fails To Achieve Orbit . 12 Failure Investigation Teams . 14 Failure Investigation Begins . .14 Hughes’ Export Administrators Deal with the Licensing Question . 17 A ‘Political’ Business Solution . 21 The Optus B3: Hughes’ Efforts to Improve the Long March Continue . 36 APSTAR 2 . .40 The Apstar 2 License . 40 The Apstar 2 Failure . 40 Failure Investigation Teams . 42 Failure Investigation Schedule . 42 The Need for a License . .42 Commerce Department Conference . 46 Same Fairing Failure Identified by Hughes . 47 A ‘Political’ Business Solution, Again? . 48 The Commerce Department Approves Data Release to the PRC . 50 SELECT COMMITTEE OF THE UNITED STATES HOUSE OF REPRESENTATIVES Hughes Tries to Get the PRC to Accept Its Findings . .. 51 CIA Analyst Visits Hughes . .. 56 A ‘Consolidated Solution’ . 58 Final Failure Investigation Report Released to the PRC by the Commerce Department . 60 Implementing the ‘Consolidated Solution’ . 64 U.S. Government Actions Following the Apstar 2 Launch Failure . 66 Defense Department Assessments of Damage to National Security . 68 Damage to National Security from the Apstar 2 Failure Investigation . 69 Damage to National Security from the Sharing of Coupled Loads Analysis . 72 Damage to National Security from Providing the PRC with Information Concerning Deficiencies in the Fairing, and Resultant Improvements to PRC Rockets and Ballistic Missiles . -
1998 Year in Review
Associate Administrator for Commercial Space Transportation (AST) January 1999 COMMERCIAL SPACE TRANSPORTATION: 1998 YEAR IN REVIEW Cover Photo Credits (from left): International Launch Services (1998). Image is of the Atlas 2AS launch on June 18, 1998, from Cape Canaveral Air Station. It successfully orbited the Intelsat 805 communications satellite for Intelsat. Boeing Corporation (1998). Image is of the Delta 2 7920 launch on September 8, 1998, from Vandenberg Air Force Base. It successfully orbited five Iridium communications satellites for Iridium LLP. Lockheed Martin Corporation (1998). Image is of the Athena 2 awaiting its maiden launch on January 6, 1998, from Spaceport Florida. It successfully deployed the NASA Lunar Prospector. Orbital Sciences Corporation (1998). Image is of the Taurus 1 launch from Vandenberg Air Force Base on February 10, 1998. It successfully orbited the Geosat Follow-On 1 military remote sensing satellite for the Department of Defense, two Orbcomm satellites and the Celestis 2 funerary payload for Celestis Corporation. Orbital Sciences Corporation (1998). Image is of the Pegasus XL launch on December 5, 1998, from Vandenberg Air Force Base. It successfully orbited the Sub-millimeter Wave Astronomy Satellite for the Smithsonian Astrophysical Observatory. 1998 YEAR IN REVIEW INTRODUCTION INTRODUCTION In 1998, U.S. launch service providers conducted In addition, 1998 saw continuing demand for 22 launches licensed by the Federal Aviation launches to deploy the world’s first low Earth Administration (FAA), an increase of 29 percent orbit (LEO) communication systems. In 1998, over the 17 launches conducted in 1997. Of there were 17 commercial launches to LEO, 14 these 22, 17 were for commercial or international of which were for the Iridium, Globalstar, and customers, resulting in a 47 percent share of the Orbcomm LEO communications constellations.