{PDF EPUB} the Rocket Men Vostok and Voskhod the First Soviet Manned Spaceflights by Rex D

Total Page:16

File Type:pdf, Size:1020Kb

{PDF EPUB} the Rocket Men Vostok and Voskhod the First Soviet Manned Spaceflights by Rex D Read Ebook {PDF EPUB} The Rocket Men Vostok And Voskhod The First Soviet Manned Spaceflights by Rex D. Hall Could the CIA have prevented the Apollo 1 fire? The 40th anniversary of NASA’s first space-related fatal accident, the Apollo 1 fire on January 27, 1967, is an opportunity to consider one of the myths that have grown up around the tragedy: the claim that the CIA might have prevented the Apollo fire. As if foreshadowing the Apollo 1 fire, the first documented fire-related fatality in a space program also occurred during a simulation. On March 23, 1961, a flash fire in an oxygen-saturated isolation chamber took the life of cosmonaut-trainee Valentin Bondarenko, at age 23 the youngest member of the year-old cosmonaut team. His death came during a routine training and medical screening activity. Published sources (references 1 and 2) differ on the details, but Bondarenko was the seventeenth cosmonaut trainee to spend ten days or more in the chamber in the previous year. The chamber atmosphere was high in oxygen content because decompression was among the stresses in store for the trainees. When he used an alcohol-soaked cotton swab to remove the adhesive residue from medical sensors on his body, and then casually discarded the swab, it fell on a electrical element used for heating food in the oxygen-rich environment and sparked a flash fire that engulfed him; he died within hours from burns over 90 percent of his body. After a rigorous investigation, testing resumed, and a few weeks later, two more trainees successfully completed the test; the next year the first women cosmonaut-trainees did, too. No sooner had Bondarenko’s tragedy permeated the Western space consciousness than the question arose: could the Apollo fire have been avoided if only the Soviet Union had been forthcoming about Bondarenko’s fate earlier? Less than three weeks later, the historic orbital flight of Bondarenko’s colleague, Yuri Gagarin, in the first Vostok spacecraft challenged America’s sense of technological superiority, and moved President Kennedy to set the national goal that became the Apollo program. Soviet-era secrecy being what it was—especially if the news did not reflect favorably on the Soviet Union—word of Bondarenko’s death didn’t reach the West until 1986. That was the year of the second American spacecraft disaster, the loss of Challenger and her crew just moments after launch. (Space aficionados shuddered at the eerie similarity of the date, January 28, 1986, with that of the Apollo 1 fire.) No sooner had Bondarenko’s tragedy permeated the Western space consciousness than the question arose: could the Apollo fire have been avoided if only the Soviet Union had been forthcoming about Bondarenko’s fate earlier? Perhaps, the thinking went, such an object lesson might have influenced NASA to design its Apollo spacecraft to use a two-gas (nitrogen and oxygen) cabin atmosphere, instead of the pure oxygen atmosphere already in use in the Mercury capsules. Or, at the very least, surely NASA would have avoided the cabin leak check procedure that required pressurizing the cabin above sea level pressure, at least not with pure oxygen. Cosmonaut Alexei Leonov, no stranger to near-death experience himself, even posited that the CIA must have successfully pierced Soviet secrecy, learned of Bondarenko’s death, and informed NASA, but that the space agency still stubbornly refused to change the gas mixture. In fact, the decision to adopt a pure oxygen atmosphere for Apollo was vigorously debated by spacecraft manufacturers and government and academic clinicians before it was finalized by NASA as a weight-saving step. And as for object lessons, there was no shortage of them, even without the CIA’s help. NASA could also have taken warning from at least seven examples of oxygen-related fires in operational US testing facilities (reference 3), four of which occurred between two years and nine months before the Apollo fire. Three involved unmanned tests of Apollo life support systems, at least one of which used pure oxygen at the planned cabin pressure of five pounds per square inch. The remaining four fire events took place during manned US Air Force and US Navy chamber tests in the late 1950s and 1962. Three of those were tests of cabin atmospheres planned for Mercury and Gemini, and their crews escaped with injuries ranging from smoke inhalation to first and second degree burns. The fourth, in early 1965, saw two Navy divers die in a fire in a chamber pressurized to 8.6 atmospheres. In this case, the pressure and gas combination was being investigated for use in deep ocean operations, not space flight. (These events—but not the Bondarenko fatality—and about 70 chamber fires since then are reviewed in reference 4.) That NASA failed to grasp the lessons of those fires is regrettable, but it was not unusual. Only four days after the Apollo fire, the Air Force lost two veterinary technicians in a pure oxygen chamber fire. Clearly NASA’s own object lesson was lost on the Air Force as well. Notwithstanding all of the foregoing, is it still possible that NASA, if it had truly known of Bondarenko’s fate, might have been motivated to modify, if not the design of the Apollo life support system, then at least the ground test protocol to eliminate the high-pressure, pure-oxygen environment that made the Apollo fire so devastating? In fact, we have two examples of ill-advised decisions that the Soviet space program made, identified and corrected, in full public view, which NASA did not formalize in its own engineering requirements for years. The first involved a means of extricating crewmembers from a spacecraft in case of a launch gone badly. In 1964 and 1965, the Soviets flew two manned Voskhod spacecraft (hurriedly modified Vostoks, rechristened to obscure their origin) to preempt NASA’s upcoming Gemini series by claiming the first multi-man flight (the three men aboard the first Voskhod trumped Gemini’s two-man capacity) and the first spacewalk (by Leonov on Voskhod 2). Both Voskhods lacked a means of escaping from the rocket booster if it went out of control soon after launch. All of the previous Vostoks carried ejection seats, and all subsequent Soyuz piloted launches have had launch-escape rockets, one of which actually saved a crew from a booster explosion on the launch pad in 1983. But the absence of a launch-escape technique aboard the Voskhods (the ejection seat was eliminated so the same spherical capsule could hold more than one cosmonaut) prompted disdain in the West—until 1983, when NASA’s Space Shuttle vehicle started flying without any means of extracting its crews during a failed launch. NASA finally experienced its first shuttle launch disaster when it lost the Challenger crew in 1986. Subsequent shuttle missions have carried a rudimentary bail-out capability for use only during landing, but any more thorough escape capabilities will not be available until 2014, when an entirely new NASA spacecraft, Orion, begins flying. We have two examples of ill-advised decisions that the Soviet space program made, identified and corrected, in full public view, which NASA did not formalize in its own engineering requirements for years. The second example involves astronaut pressure suits as a back-up in case cabin pressure is lost during launch or landing. The first Voskhod and the first ten Soyuz missions carried their cosmonaut crews wearing only garments similar to tracksuits. After the Soyuz 11 crew died during a re- entry cabin depressurization in 1971, subsequent Soyuz capsules were modified so all cosmonauts could wear lightweight full-pressure suits. Thankfully, no crews have needed this layer of protection since then. However, NASA did not provide similar “launch and entry suits” until the Challenger loss prompted more thoughtful consideration of the various scenarios in which such protection might afford the crews a better chance of survival. However, it must be noted that during the Apollo flights, American astronauts wore space suits during launch and major maneuvers; after Soyuz 11, NASA even considered reinforcing its suit-wearing policy on the remaining Apollo lunar missions, but determined that other measures already in place were adequate. Still, in the Shuttle era, Russian evidence supporting the need for pressure suits during launch and reentry was apparently not considered sufficient by NASA for another 15 years after the loss of the Soyuz 11 crew. The anniversaries of space tragedies are rightly a time to consider the unique causes and effects that lead to terrible losses. The loss of the Columbia and her crew during reentry in 2003, from damage incurred during launch but not detected until long after the accident, came only days after the Apollo and Challenger anniversaries, another chilling coincidence. However, it prompted a reexamination of national space policy, leading to the decision to end the Space Shuttle program and initiate the Orion program, designed to be less susceptible to the launch-phase failures of the Shuttle. Thus, there is evidence that the NASA of the 21st century has learned from object lessons of the past. For example, NASA’s White Sands Test Facility excels in testing and evaluating potentially hazardous materials for space flight (reference 5). But, if the NASA of the 1960s, 1970’s, and 1980’s was unable to generalize from knowledge of its own object lessons and those of the Air Force and Navy, let alone those publicly known from the Soviet Union, we cannot expect that the knowledge of one more such lesson, even one as graphic as Bondarenko’s death, would have made a difference.
Recommended publications
  • Soviet Steps Toward Permanent Human Presence in Space
    SALYUT: Soviet Steps Toward Permanent Human Presence in Space December 1983 NTIS order #PB84-181437 Recommended Citation: SALYUT: Soviet Steps Toward Permanent Human Presence in Space–A Technical Mere- orandum (Washington, D. C.: U.S. Congress, Office of Technology Assessment, OTA- TM-STI-14, December 1983). Library of Congress Catalog Card Number 83-600624 For sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402 Foreword As the other major spacefaring nation, the Soviet Union is a subject of interest to the American people and Congress in their deliberations concerning the future of U.S. space activities. In the course of an assessment of Civilian Space Stations, the Office of Technology Assessment (OTA) has undertaken a study of the presence of Soviets in space and their Salyut space stations, in order to provide Congress with an informed view of Soviet capabilities and intentions. The major element in this technical memorandum was a workshop held at OTA in December 1982: it was the first occasion when a significant number of experts in this area of Soviet space activities had met for extended unclassified discussion. As a result of the workshop, OTA prepared this technical memorandum, “Salyut: Soviet Steps Toward Permanent Human Presence in Space. ” It has been reviewed extensively by workshop participants and others familiar with Soviet space activities. Also in December 1982, OTA wrote to the U. S. S. R.’s Ambassador to the United States Anatoliy Dobrynin, requesting any information concerning present and future Soviet space activities that the Soviet Union judged could be of value to the OTA assess- ment of civilian space stations.
    [Show full text]
  • Praxis Manned Spaceflight Log 1961±2006
    Praxis Manned Space¯ight Log 1961±2006 Tim Furniss and David J. Shayler with Michael D. Shayler Praxis Manned Spaceflight Log 1961±2006 Published in association with PPraxisraxis PPublishiublishingng Chichester, UK Tim Furniss David J. Shayler Space¯ight Correspondent Astronautical Historian Flight International Astro Info Service Bideford Halesowen Devon West Midlands UK UK Michael D. Shayler Editor and Designer Astro Info Service Birmingham UK SPRINGER±PRAXIS BOOKS IN SPACE EXPLORATION SUBJECT ADVISORY EDITOR: John Mason B.Sc., M.Sc., Ph.D. ISBN 10: 0-387-34175-7 Springer Berlin Heidelberg New York ISBN 13: 978-0-387-34175-0 Springer Berlin Heidelberg New York Springer is part of Springer-Science + Business Media (springer.com) Library of Congress Control Number: 2006937359 Apart from any fair dealing for the purposes of research or private study, or criticism or review, as permitted under the Copyright, Designs and Patents Act 1988, this publication may only be reproduced, stored or transmitted, in any form or by any means, with the prior permission in writing of the publishers, or in the case of reprographic reproduction in accordance with the terms of licences issued by the Copyright Licensing Agency. Enquiries concerning reproduction outside those terms should be sent to the publishers. # Praxis Publishing Ltd, Chichester, UK, 2007 Printed in Germany The use of general descriptive names, registered names, trademarks, etc. in this publication does not imply, even in the absence of a speci®c statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. Cover design: Jim Wilkie Project Copy Editor: Mike Shayler Typesetting: Originator Publishing Services, Gt Yarmouth, Norfolk, UK Printed on acid-free paper Contents Authors' Preface ......................................
    [Show full text]
  • Limitations of Spacecraft Redundancy: a Case Study Analysis
    44th International Conference on Environmental Systems Paper Number 13-17 July 2014, Tucson, Arizona Limitations of Spacecraft Redundancy: A Case Study Analysis Robert P. Ocampo1 University of Colorado Boulder, Boulder, CO, 80309 Redundancy can increase spacecraft safety by providing the crew or ground with multiple means of achieving a given function. However, redundancy can also decrease spacecraft safety by 1) adding additional failure modes to the system, 2) increasing design “opaqueness”, 3) encouraging operational risk, and 4) masking or “normalizing” design flaws. Two Loss of Crew (LOC) events—Soyuz 11 and Challenger STS 51-L—are presented as examples of these limitations. Together, these case studies suggest that redundancy is not necessarily a fail-safe means of improving spacecraft safety. I. Introduction A redundant system is one that can achieve its intended function through multiple independent pathways or Aelements 1,2. In crewed spacecraft, redundancy is typically applied to systems that are critical for safety and/or mission success3,4. Since no piece of hardware can be made perfectly reliable, redundancy—in theory—allows for the benign (e.g. non-catastrophic) failure of critical elements. Redundant elements can be 1) similar or dissimilar to each other, 2) activated automatically (“hot spare”) or manually (“cold spare”), and 3) located together or separated geographically5-7. U.S. spacecraft have employed redundancy on virtually all levels of spacecraft design, from component to subsystem7,8. Redundancy has a successful history of precluding critical and catastrophic failures during human spaceflight. A review of NASA mission reports, from Mercury to Space Shuttle, indicates that redundancy has saved the crew or extended the mission over 160 times, or roughly once per flight9.
    [Show full text]
  • Rex D. Hall and David J. Shayler
    Rex D. Hall and David J. Shayler Soyuz A Universal Spacecraft ruuiiMicPublishedu 11in1 aaaundiiuiassociationi witwimh ^^ • Springer Praxis Publishing PRHB Chichester, UK "^UF Table of contents Foreword xvii Authors' preface xix Acknowledgements xxi List of illustrations and tables xxiii Prologue xxix ORIGINS 1 Soviet manned spaceflight after Vostok 1 Design requirements 1 Sever and the 1L: the genesis of Soyuz 3 The Vostok 7/1L Soyuz Complex 4 The mission sequence of the early Soyuz Complex 6 The Soyuz 7K complex 7 Soyuz 7K (Soyuz A) design features 8 The American General Electric concept 10 Soyuz 9K and Soyuz 1 IK 11 The Soyuz Complex mission profile 12 Contracts, funding and schedules 13 Soyuz to the Moon 14 A redirection for Soyuz 14 The N1/L3 lunar landing mission profile 15 Exploring the potential of Soyuz 16 Soyuz 7K-P: a piloted anti-satellite interceptor 16 Soyuz 7K-R: a piloted reconnaissance space station 17 Soyuz VI: the military research spacecraft Zvezda 18 Adapting Soyuz for lunar missions 20 Spacecraft design changes 21 Crewing for circumlunar missions 22 The Zond missions 23 The end of the Soviet lunar programme 33 The lunar orbit module (7K-LOK) 33 viii Table of contents A change of direction 35 References 35 MISSION HARDWARE AND SUPPORT 39 Hardware and systems 39 Crew positions 40 The spacecraft 41 The Propulsion Module (PM) 41 The Descent Module (DM) 41 The Orbital Module (OM) 44 Pyrotechnic devices 45 Spacecraft sub-systems 46 Rendezvous, docking and transfer 47 Electrical power 53 Thermal control 54 Life support 54
    [Show full text]
  • The Soviet Space Program
    C05500088 TOP eEGRET iuf 3EEA~ NIE 11-1-71 THE SOVIET SPACE PROGRAM Declassified Under Authority of the lnteragency Security Classification Appeals Panel, E.O. 13526, sec. 5.3(b)(3) ISCAP Appeal No. 2011 -003, document 2 Declassification date: November 23, 2020 ifOP GEEAE:r C05500088 1'9P SloGRET CONTENTS Page THE PROBLEM ... 1 SUMMARY OF KEY JUDGMENTS l DISCUSSION 5 I. SOV.IET SPACE ACTIVITY DURING TfIE PAST TWO YEARS . 5 II. POLITICAL AND ECONOMIC FACTORS AFFECTING FUTURE PROSPECTS . 6 A. General ............................................. 6 B. Organization and Management . ............... 6 C. Economics .. .. .. .. .. .. .. .. .. .. .. ...... .. 8 III. SCIENTIFIC AND TECHNICAL FACTORS ... 9 A. General .. .. .. .. .. 9 B. Launch Vehicles . 9 C. High-Energy Propellants .. .. .. .. .. .. .. .. .. 11 D. Manned Spacecraft . 12 E. Life Support Systems . .. .. .. .. .. .. .. .. 15 F. Non-Nuclear Power Sources for Spacecraft . 16 G. Nuclear Power and Propulsion ..... 16 Te>P M:EW TCS 2032-71 IOP SECl<ET" C05500088 TOP SECRGJ:. IOP SECREI Page H. Communications Systems for Space Operations . 16 I. Command and Control for Space Operations . 17 IV. FUTURE PROSPECTS ....................................... 18 A. General ............... ... ···•· ................. ····· ... 18 B. Manned Space Station . 19 C. Planetary Exploration . ........ 19 D. Unmanned Lunar Exploration ..... 21 E. Manned Lunar Landfog ... 21 F. Applied Satellites ......... 22 G. Scientific Satellites ........................................ 24 V. INTERNATIONAL SPACE COOPERATION ............. 24 A. USSR-European Nations .................................... 24 B. USSR-United States 25 ANNEX A. SOVIET SPACE ACTIVITY ANNEX B. SOVIET SPACE LAUNCH VEHICLES ANNEX C. SOVIET CHRONOLOGICAL SPACE LOG FOR THE PERIOD 24 June 1969 Through 27 June 1971 TCS 2032-71 IOP SLClt~ 70P SECRE1- C05500088 TOP SEGR:R THE SOVIET SPACE PROGRAM THE PROBLEM To estimate Soviet capabilities and probable accomplishments in space over the next 5 to 10 years.' SUMMARY OF KEY JUDGMENTS A.
    [Show full text]
  • Building and Maintaining the International Space Station (ISS)
    / Building and maintaining the International Space Station (ISS) is a very complex task. An international fleet of space vehicles launches ISS components; rotates crews; provides logistical support; and replenishes propellant, items for science experi- ments, and other necessary supplies and equipment. The Space Shuttle must be used to deliver most ISS modules and major components. All of these important deliveries sustain a constant supply line that is crucial to the development and maintenance of the International Space Station. The fleet is also responsible for returning experiment results to Earth and for removing trash and waste from the ISS. Currently, transport vehicles are launched from two sites on transportation logistics Earth. In the future, the number of launch sites will increase to four or more. Future plans also include new commercial trans- ports that will take over the role of U.S. ISS logistical support. INTERNATIONAL SPACE STATION GUIDE TRANSPORTATION/LOGISTICS 39 LAUNCH VEHICLES Soyuz Proton H-II Ariane Shuttle Roscosmos JAXA ESA NASA Russia Japan Europe United States Russia Japan EuRopE u.s. soyuz sL-4 proton sL-12 H-ii ariane 5 space shuttle First launch 1957 1965 1996 1996 1981 1963 (Soyuz variant) Launch site(s) Baikonur Baikonur Tanegashima Guiana Kennedy Space Center Cosmodrome Cosmodrome Space Center Space Center Launch performance 7,150 kg 20,000 kg 16,500 kg 18,000 kg 18,600 kg payload capacity (15,750 lb) (44,000 lb) (36,400 lb) (39,700 lb) (41,000 lb) 105,000 kg (230,000 lb), orbiter only Return performance
    [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]
  • Association of Space Explorers XXII Planetary Congress Prague, Czech Republic 2009
    Association of Space Explorers XXII Planetary Congress Prague, Czech Republic 2009 Commemorative Poster Signature Key Viktor Afanasyev Vladimir Aksyonov Alexander Alexandrov Soyuz TM-11, Soyuz TM-18, Soyuz 22, Soyuz T-2 Soyuz T-9, Soyuz TM-3 Soyuz TM-29, Soyuz TM-33 Alexander Alexandrov Sergei Avdeev Alexander Balandin Soyuz TM-5 Soyuz TM-15, Soyuz TM-22, Soyuz TM-9 Soyuz TM-28 Yuri Baturin Karol Bobko Vance Brand Soyuz TM-28, Soyuz TM-32 STS 6, STS 51D, STS 51J ASTP, STS 5, STS 41B, STS 35 Jean-François Clervoy Roger Crouch Reinhold Ewald STS 66, STS 84, STS 103 STS 83, STS 94 Soyuz TM-25 John Fabian Bertalan Farkas Anatoli Filipchenko STS 7, STS 51G Soyuz 36 Soyuz 36 Jake Garn Owen Garriott Richard Garriott STS 51D Skylab 3, STS 9 Soyuz TMA-13 Georgi Grechko Chris Hadfield Henry Hartsfield Soyuz 17, Soyuz 26, Soyuz T-14 STS 74, STS 100 STS 4, STS 41D, STS 61A Miroslaw Hermaszewski Georgi Ivanov Oleg Kotov Soyuz 30 Soyuz 33 Soyuz TMA-10, Soyuz TMA-17., Expedition 22 Alexei Leonov Vladimir Lyakhov Pam Melroy Voskhod 2, ASTP Soyuz 32, Soyuz T-9, STS 92, STS 112, STS 120 Soyuz TM-6 Dumitru-Dorin Prunariu Kenneth Reightler, Jr. Vladimir Remek Soyuz 40 STS 48, STS 60 Soyuz 28 Richard Richards Viktor Savinykh Rusty Schweickart STS 28, STS 41, STS 50, STS 64 Soyuz T-4, Soyuz T-13, Soyuz Apollo 9 TM-5 Alexander Serebrov Vladimir Shatalov Yuri Usachev Soyuz T-7, Soyuz T-8, Soyuz Soyuz 4, Soyuz 8, Soyuz 10 Soyuz TM-18, Soyuz TM-23, TM-8, Soyuz TM-17 STS 101/Expedition 2/STS 102 Franz Viehbock Pavel Vinogradov Sergei Volkov Soyuz TM-13 Soyuz TM-26, Soyuz TMA-8/ Soyuz TMA-12, Expedition 17 Expedition 13 James Voss Charles Walker Yi Soyeon STS 44, STS 53, STS 69, STS 101/ STS 41D, STS 51D, STS 61B Soyuz TMA-12 Expedition 2/STS 102 Forty-nine astronauts and cosmonauts* from 14 nations gathered October 4-10, 2009 in Prague, Czech Republic for the XXII Planetary Congress of the Association of Space Explorers (ASE).
    [Show full text]
  • China's Space Program: an Overview
    Order Code RS21641 Updated October 18, 2005 CRS Report for Congress Received through the CRS Web China’s Space Program: An Overview Marcia S. Smith Specialist in Aerospace and Telecommunications Policy Resources, Science, and Industry Division Summary The People’s Republic of China successfully completed its second human spaceflight mission on October 17, 2005. China is only the third country, after Russia and the United States, able to launch people into space. Its first human spaceflight was in 2003 when a single astronaut, or “taikonaut,” made a flight lasting slightly less than a day. The 2005 flight lasted five days, and involved two taikonauts. As the United States embarks upon President Bush’s “Vision for Space Exploration” to return astronauts to the Moon by 2020 and someday send them to Mars, some may view China’s entrance into the human exploration of space as a competitive threat, while others may view China as a potential partner. This report will be updated as warranted. Introduction China has been launching satellites since 1970. Most of the launches are of Chinese communications, weather, remote sensing, navigation, or scientific satellites. Some of those satellites may be for military applications, or are dual use. Some were commercial launches for foreign countries or companies, primarily placing communications satellites into orbit. China launched its first astronaut, or “taikonaut,”1 in October 2003. China has three space launch sites: Jiuquan (also called Shuang Cheng-tzu) in the Gobi desert; Xichang, in southeastern China (near Chengdu); and Taiyuan, south of Beijing. Jiuquan was China’s first launch site, and is used for launches of a variety of spacecraft, including those related to the human spaceflight program.
    [Show full text]
  • Apollo-Soyuz Test Project
    --.I m ...ir,,.= The document_-contains materials on the Soyuz-Apollo test and consists of two parts, prepared by the USSR and USA sides res- pectively. Both parts outline the purposes and program of the mission, the spacecraft design, the flight plan and information on Joint and unilateral scientific experiments. Brief biographies of the cosmonauts and astronauts, the Joint mission crew members_ are also presented. The document covers technical support activities providing mission control and gives information about the ASTP Soviet and American leaders. As the USSR and USA parts of the document have been prepared independently, there might be duplication in the sections dealing with the Joint activities. The document is intended for press representatives and various mass information means. CONTENTS Page I.0 INTRODUCTION ....................................... 10 1.1 Background ......................................... I0 1,2 Apollo-Soyuz joint test project objectives .......... 13 2.0 COMPATIBILITY PROBLEMS ................... ......... • 15 2.1 Spacecraft compatibility conditions and principal solutions accepted for Apollo-Ssyuz Test Mission .... 15 2.2 Compatibility of ground flight control personnel ... 18 2_3 Methodological compatibility ....................... 20 3.0 SOYUZ SPACECRAFT ................................... 22 3.1 PurPose. Brief data on Soyuz spacecraft flights .... 22 3.2 Soyuz spacecraft description ....................... 25 3.2.1 General description of the Soyuz spacecraft.. 25 Main characteristics ........................
    [Show full text]
  • Spaceport News America’S Gateway to the Universe
    July 28, 2000 Vol. 39, No. 15 Spaceport News America’s gateway to the universe. Leading the world in preparing and launching missions to Earth and beyond. http://www-pao.ksc.nasa.gov/kscpao/snews/snewstoc.htm John F. Kennedy Space Center Zvezda takes flight Launch of key component heralds new phase of International Space Station Destined to transform the for the Station. International Space Station into a At press time, the module was new home in orbit, the Russian- operating well in an orbit with a built Zvezda living quarters high point of about 221 statute module lifted off flawlessly from the miles and a low point of 115 Baikonur Cosmodrome, Kazakh- statute miles. stan, at 12:56 a.m. on July 15. Flight controllers at the Russian Only 15 minutes after its launch Mission Control Center in aboard a Russian Proton booster, Korolev, Russia, were continuing the new module was safely in orbit, to activate and check out the with its antennas, solar arrays and module’s systems, fire its engines other exterior equipment perfectly periodically to adjust its orbit, and extended. prepare for a docking with the In addition to serving as the Space Station. early station living quarters, The Station was set to begin a Zvezda will be the main docking final rendezvous with Zvezda, port for Russian Progress cargo culminating in a docking planned resupply vehicles. It also will at about 8:45 p.m. July 25. At top, a Proton rocket lifts the Zvezda module from the Baikonur provide early propulsive attitude Cosmodrome, Kazakhstan.
    [Show full text]
  • Part 2 Almaz, Salyut, And
    Part 2 Almaz/Salyut/Mir largely concerned with assembly in 12, 1964, Chelomei called upon his Part 2 Earth orbit of a vehicle for circumlu- staff to develop a military station for Almaz, Salyut, nar flight, but also described a small two to three cosmonauts, with a station made up of independently design life of 1 to 2 years. They and Mir launched modules. Three cosmo- designed an integrated system: a nauts were to reach the station single-launch space station dubbed aboard a manned transport spacecraft Almaz (“diamond”) and a Transport called Siber (or Sever) (“north”), Logistics Spacecraft (Russian 2.1 Overview shown in figure 2-2. They would acronym TKS) for reaching it (see live in a habitation module and section 3.3). Chelomei’s three-stage Figure 2-1 is a space station family observe Earth from a “science- Proton booster would launch them tree depicting the evolutionary package” module. Korolev’s Vostok both. Almaz was to be equipped relationships described in this rocket (a converted ICBM) was with a crew capsule, radar remote- section. tapped to launch both Siber and the sensing apparatus for imaging the station modules. In 1965, Korolev Earth’s surface, cameras, two reentry 2.1.1 Early Concepts (1903, proposed a 90-ton space station to be capsules for returning data to Earth, 1962) launched by the N-1 rocket. It was and an antiaircraft cannon to defend to have had a docking module with against American attack.5 An ports for four Soyuz spacecraft.2, 3 interdepartmental commission The space station concept is very old approved the system in 1967.
    [Show full text]