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Contingency Shuttle Crew Support (Cscs)/Rescue Flight Resource Book
CSCS/Rescue Flight Resource Book JSC-62900 CONTINGENCY SHUTTLE CREW SUPPORT (CSCS)/RESCUE FLIGHT RESOURCE BOOK OVERVIEW 1 Mission Operations CSCS 2 Directorate RESCUE 3 FLIGHT DA8/Flight Director Office Final July 12, 2005 National Aeronautics and Space Administration Lyndon B. Johnson Space Center Houston, Texas FINAL 07/12/05 2-i Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 CONTINGENCY SHUTTLE CREW SUPPORT (CSCS)/RESCUE FLIGHT RESOURCE BOOK FINAL JULY 12, 2005 PREFACE This document, dated May 24, 2005, is the Basic version of the Contingency Shuttle Crew Support (CSCS)/Rescue Flight Resource Book. It is requested that any organization having comments, questions, or suggestions concerning this document should contact DA8/Book Manager, Flight Director Office, Building 4 North, Room 3039. This is a limited distribution and controlled document and is not to be reproduced without the written approval of the Chief, Flight Director Office, mail code DA8, Lyndon B. Johnson Space Center, Houston, TX 77058. FINAL 07/12/05 2-ii Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 1.0 - OVERVIEW Section 1.0 is the overview of the entire Contingency Shuttle Crew Support (CSCS)/Rescue Flight Resource Book. FINAL 07/12/05 2-iii Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 This page intentionally blank. FINAL 07/12/05 2-iv Verify this is the correct version before using. CSCS/Rescue Flight Resource Book JSC-62900 2.0 - CONTINGENCY SHUTTLE CREW SUPPORT (CSCS) 2.1 Procedures Overview.......................................................................................................2-1 2.1.1 ................................................................................ -
Modèle Document
AVISO DT CorSSH and DT SLA Product Handbook Reference: CLS-DOS-NT-08.341 Nomenclature: - Issue: 2 rev 0 Date: October 2012 Aviso Altimetry 8-10 rue Hermès, 31520 Ramonville St Agne, France – [email protected] DT CorSSH and DT SLA Product Handbook CLS-DOS-NT-08.341 Iss :2.9 - date : 28/02/2012 - Nomenclature: - i.1 Chronology Issues: Issue: Date: Reason for change: 1.0 2005/07/18 1st issue 1.1 2005/11/08 Processing of ERS-2 data 1.2 2005/10/17 Processing of GFO data 1.3 2008/06/10 New standards for corrections and models for Jason-1 1.4 2008/08/07 New standards for corrections and models for Envisat after cycle 65. 1.5 2008/12/18 New standards for corrections and models for Jason-1 GDR-C. 1.6 2010/03/05 New standards for Jason-2 1.7 2010/06/08 New standards for corrections and/or models Processing of ERS-1 data 1.8 2011/04/14 Correction of table 2 1.9 2012/02/28 Specification of the reading routines for SLA files only 2.0 2012/10/16 New geodetic orbit for Jason-1 (c≥500) New version D for Jason-2 (c≥146) D : page deleted I : page inserted M : page modified DT CorSSH and DT SLA Product Handbook CLS-DOS-NT-08.341 Iss :2.9 - date : 28/02/2012 - Nomenclature: - i.2 List of Acronyms: ATP Along Track Product Aviso Archiving, Validation and Interpretation of Satellite Oceanographic data Cersat Centre ERS d’Archivage et de Traitement CLS Collecte, Localisation, Satellites CMA Centre Multimissions Altimetriques Cnes Centre National d’Etudes Spatiales CorSSH Corrected Sea Surface Height Doris Doppler Orbitography and Radiopositioning Integrated -
Measurements of Π , K , P and ¯P Spectra in Proton-Proton
EUROPEAN ORGANISATION FOR NUCLEAR RESEARCH (CERN) Submitted to: Eur. Phys. J. C CERN-EP-2017-066 September 28, 2017 Measurements of π±,K±, p and ¯p spectra in proton-proton interactions at 20, 31, 40, 80 and 158 GeV=c with the NA61/SHINE spectrometer at the CERN SPS The NA61/SHINE Collaboration Measurements of inclusive spectra and mean multiplicities of π±,K±, p and p¯ produced in =c inelasticp p+p interactions at incident projectile momenta of 20, 31, 40, 80 and 158 GeV ( s = 6.3, 7.7, 8.8, 12.3 and 17.3 GeV, respectively) were performed at the CERN Super Proton Synchrotron using the large acceptance NA61/SHINE hadron spectrometer. Spectra are presented as function of rapidity and transverse momentum and are compared to predictions of current models. The measurements serve as the baseline in the NA61/SHINE study of the properties of the onset of deconfinement and search for the critical point of strongly interacting matter. arXiv:1705.02467v2 [nucl-ex] 27 Sep 2017 © 2017 CERN for the benefit of the NA61/SHINE Collaboration. Reproduction of this article or parts of it is allowed as specified in the CC-BY-4.0 license. 1. Introduction This paper presents experimental results on inclusive spectra and mean multiplicities of π±,K±, p and p¯ produced in inelastic p+p interactions at 20, 31, 40, 80 and 158 GeV=c. The measurements were performed by the multi-purpose NA61/SHINE experiment [1, 2] at the CERN Super Proton Synchrotron (SPS). The new measurements complement previously published results from the same datasets on π− production [3] obtained without particle identification as well as on fluctuations of charged particles [4]. -
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. -
Classification of Geosynchronous Objects Issue 12
EUROPEAN SPACE AGENCY EUROPEAN SPACE OPERATIONS CENTRE GROUND SYSTEMS ENGINEERING DEPARTMENT Space Debris Office CLASSIFICATION OF GEOSYNCHRONOUS OBJECTS ISSUE 12 by R. Choc and R. Jehn Produced with the DISCOS Database February 2010 ESOC Robert-Bosch-Str. 5, 64293 Darmstadt, Germany 3 Abstract This is a status report on geosynchronous objects as of the end of 2009. Based on orbital data in ESA’s DISCOS database and on orbital data provided by KIAM the situation near the geostationary ring (here defined as orbits with mean motion between 0.9 and 1.1 revolutions per day, eccentricity smaller than 0.2 and inclination below 30 deg) is analysed. From 1161 objects for which orbital data are available, 391 are controlled inside their longitude slots, 594 are drifting above, below or through GEO, 169 are in a libration orbit and 7 whose status could not be determined. Furthermore, there are 77 uncontrolled objects without orbital data (of which 66 have not been catalogued). Thus the total number of known objects in the geostationary region is 1238. During 2009 twenty-one spacecraft reached end-of-life. Eleven of them were reorbited following the IADC recommendations, one spacecraft was reorbited with a perigee of 225 km - it is not yet clear if it will enter the 200-km protected zone around GEO or not -, six spacecraft were reorbited too low and three spacecraft did not or could not make any reorbiting manouevre at all and are now librating inside the geostationary ring. If you detect any error or if you have any comment or question please contact R¨udiger Jehn European Space Operations Center Robert-Bosch-Str. -
The ASTRA Satellite System the ASTRA Satellite System at 19.2° East Services on ASTRA (September 2000)
Société Européenne des Satellites SES in brief (I) u Operator of ASTRA, the leading DTH satellite system in Europe u Satellite fleet: è 9 satellites in operation (7 at 19.2° East, 2 at 28.2° East) è 4 additional satellites until end of year 2001 u ASTRA carries more than 600 digital and analogue TV services and 389 radio services of leading European and international broadcasters for Europe's main language markets u ASTRA audience exceeds 79 million households in 22 European countries SES in brief (II) u Company listed on Luxembourg and Frankfurt Stock Exchanges èinstitutional and private shareholders èLuxembourg State holds 16.67 % of equity è33% of capital floated on Stock Exchange u Operating under a concession agreement with the Luxembourg State u 426 employees of 20 different nations u Turnover 1999: EUR 725.2 million H1 2000: EUR 403.0 million The ASTRA Satellite System The ASTRA Satellite System at 19.2° East Services on ASTRA (September 2000) 19.2° East u 85 analogue TV services for the German, English and pan- European market u 324 digital TV services for the French, German, More than -to-air Spanish, Dutch, Polish, Italian, Luxembourgish 75 free and pan-European market TV services u 313 analogue and digital radio services 28.2° East u 207 digital TV services for the UK and Ireland u 72 digital audio services for the UK and Ireland ASTRA coverage in Europe* (Mid Year 1992 to 2000) 90 80 70 60 50 40 30 20 ASTRA Households in Mill. 10 0 1992 1993 1994 1995 1996 1997 1998 1999 2000 DTH&SMATV 9.77 13.87 16.71 21.43 22.03 23.57 25.83 27.92 29.04 Cable 26.98 31.33 36.44 37.49 41.97 44.70 47.61 49.05 50.20 *22 European countries within the ASTRA footprint Source: SES/ASTRA, Satellite Monitors SES/ASTRA, Market Information Group, August 2000 Forecast of European DTH/SMATV Households 1997 – 2010 DTH/SMATV Households in Mill. -
Proton Accident with GLONASS Satellites
3/29/2018 Proton accident with GLONASS satellites Previous Proton mission: SES6 PICTURE GALLERY A Proton rocket with the Block D 11S861 stage and 813GLN34 payload firing shortly before liftoff on July 2, 2013. Upcoming book on space exploration Read more and watch videos in: Site map Site update log About this site About the author The illfated Proton rocket lifts off on July 2, 2013, at 06:38:21.585 Moscow Time (July 1, 10:38 p.m. EDT). The rocket crashed approximately 32.682 seconds later, Roskosmos said on July 18, 2013. Mailbox Russia's Proton crashes with a trio of navigation satellites SUPPORT THIS SITE! Published: July 1; updated: July 2, 3, 4, 5, 9, 11, 15, 18, 19; 23; Aug. 11 Related pages: Russia's Proton rocket crashed less than a minute after its liftoff from Baikonur, Kazakhstan. A ProtonM vehicle No. 53543 with a Block DM03 (11S86103) upper stage lifted off as scheduled from Pad No. 24 at Site 81 (launch complex 8P882K) in Baikonur Cosmodrome on July 2, 2013, at 06:38:21.585 Moscow Time (on July 1, 10:38 p.m. EDT). The rocket started veering off course right after leaving the pad, deviating from the vertical path in various RD253/275 engines directions and then plunged to the ground seconds later nose first. The payload section and the upper stage were sheered off the vehicle moments before it impacted the ground and exploded. The flight lasted no more than 30 seconds. Searching for details: The Russian space agency's ground processing and launch contractor, TsENKI, was broadcasting the launch live and captured the entire process of the vehicle's disintegration and its crash. -
Space Almanac 2007
2007 Space Almanac The US military space operation in facts and figures. Compiled by Tamar A. Mehuron, Associate Editor, and the staff of Air Force Magazine 74 AIR FORCE Magazine / August 2007 Space 0.05g 60,000 miles Geosynchronous Earth Orbit 22,300 miles Hard vacuum 1,000 miles Medium Earth Orbit begins 300 miles 0.95g 100 miles Low Earth Orbit begins 60 miles Astronaut wings awarded 50 miles Limit for ramjet engines 28 miles Limit for turbojet engines 20 miles Stratosphere begins 10 miles Illustration not to scale Artist’s conception by Erik Simonsen AIR FORCE Magazine / August 2007 75 US Military Missions in Space Space Support Space Force Enhancement Space Control Space Force Application Launch of satellites and other Provide satellite communica- Ensure freedom of action in space Provide capabilities for the ap- high-value payloads into space tions, navigation, weather infor- for the US and its allies and, plication of combat operations and operation of those satellites mation, missile warning, com- when directed, deny an adversary in, through, and from space to through a worldwide network of mand and control, and intel- freedom of action in space. influence the course and outcome ground stations. ligence to the warfighter. of conflict. US Space Funding Millions of constant Fiscal 2007 dollars 60,000 50,000 40,000 30,000 20,000 10,000 0 Fiscal Year 59 62 65 68 71 74 77 80 83 86 89 92 95 98 01 04 Fiscal Year NASA DOD Other Total Fiscal Year NASA DOD Other Total 1959 1,841 3,457 240 5,538 1983 13,051 18,601 675 32,327 1960 3,205 3,892 -
General Studies Series
IAS General Studies Series Current Affairs (Prelims), 2013 by Abhimanu’s IAS Study Group Chandigarh © 2013 Abhimanu Visions (E) Pvt Ltd. All rights reserved. No part of this document may be reproduced or transmitted in any form or by any means, electronic, mechanical, photocopying, recording, or any information storage or retrieval system or otherwise, without prior written permission of the owner/ publishers or in accordance with the provisions of the Copyright Act, 1957. Any person who does any unauthorized act in relation to this publication may be liable to criminal prosecution and civil claim for the damages. 2013 EDITION Disclaimer: Information contained in this work has been obtained by Abhimanu Visions from sources believed to be reliable. However neither Abhimanu's nor their author guarantees the accuracy and completeness of any information published herein. Though every effort has been made to avoid any error or omissions in this booklet, in spite of this error may creep in. Any mistake, error or discrepancy noted may be brought in the notice of the publisher, which shall be taken care in the next edition but neither Abhimanu's nor its authors are responsible for it. The owner/publisher reserves the rights to withdraw or amend this publication at any point of time without any notice. TABLE OF CONTENTS PERSONS IN NEWS .............................................................................................................................. 13 NATIONAL AFFAIRS .......................................................................................................................... -
Only Six Chinese Human Spaceflight Missions
Fact Sheet Updated April 29, 2021 CHINA’S HUMAN SPACEFLIGHT PROGRAM: BACKGROUND AND LIST OF CREWED AND AUTOMATED LAUNCHES China's human spaceflight program, Project 921, officially began in 1992. The program is proceeding at a measured pace. The most recent crewed launch, Shenzhou-11 in October 2016, was the 11th flight in the series, but only the sixth to carry a crew. Shenzhou Spacecraft: Shenzhou 1-4 were automated tests of the spacecraft. Shenzhou-8 was an automated test of rendezvous and docking procedures with the Tiangong-1 space station. The others (5, 6, 7, 9, 10, 11) carried crews of one, two or three people and were launched in 2003, 2005, 2008, 2012, 2013 and 2016 respectively (see list below) Space Stations: Tiangong-1, China's first space station, was launched in September 2011. It hosted the automated Shenzhou-8 in 2011 and two three-person crews: Shenzhou-9 in 2012 and Shenzhou-10 in 2013. It made an uncontrolled reentry at 8:16 pm April 1, 2018 EDT (00:16 April 2 UTC; 8:16 am April 2 Beijing Time) over the southern Pacific Ocean. Tiangong-1 was a small 8.5 metric ton (MT) module. As first space stations go, it was rather modest -- just less than half the mass of the world's first space station, the Soviet Union’s Salyut 1. Launched in 1971, Salyut 1 had a mass of about 18.6 MT. The first U.S. space station, Skylab, launched in 1973, had a mass of about 77 MT. Today's International Space Station (ISS), a partnership among the United States, Russia, Japan, Europe, and Canada, has a mass of about 400 MT and has been permanently occupied by 2-6 person crews rotating on 4-6 month missions since November 2000. -
NIDS China Security Report 2021 China’S Military Strategy in the New Era
ISBN: 978-4-86482-088-2 NIDS CHINA SECURITY REPORT NIDS China Security Report 2021 China’s Military Strategy in the New Era National Institute for Defense Studies, Japan National Institute for Defense Studies, Japan NIDS China Security Report 2021 China’s Military Strategy in the New Era Published by The National Institute for Defense Studies 5-1 Honmura-cho, Ichigaya, Shinjuku-ku, Tokyo 162-8808 Japan Website: http://www.nids.mod.go.jp Translated by INTERBOOKS Copyright © 2020 by the National Institute for Defense Studies, Japan All rights reserved. No part of this publication may be reproduced in any form without written, prior permission from the publisher. The China Security Report 2021 comprises NIDS researchers’ analyses and descriptions based on information compiled from open sources in Japan and overseas. The statements contained herein do not necessarily represent the official position of the Government of Japan or the Ministry of Defense. This publication is a translation of the Japanese version originally published in November 2020. ISBN978-4-86482-088-2 Printed in Japan NIDS China Security Report 2021 Contents Preface iii Summary v Acronyms and Abbreviations viii Introduction 2 Chapter 1: China’s Preparations for Informatized Warfare 1. Changes in China’s Military Strategy 6 (1) The Era of Mao Zedong (1927–1976): The Curse of the Final War and Active Defense 6 (2) The Era of Deng Xiaoping (1976–1989): A Break from the Final War and a Shift to Local War 7 (3) The Era of Jiang Zemin (1989–2004): Local Wars under High-Tech Conditions 9 (4) The Era of Hu Jintao (2004–2012): Informatized Local Wars 10 2. -
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 .