What Happened to Russia's Space Shuttle Program? | Photofind.Com
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Space Shuttle Program
Space Shuttle program The Space Shuttle Columbia seconds after engine ignition, 1981 (NASA). For the first two missions only, the external fuel tank spray-on foam insulation (SOFI) was painted white. Subsequent missions have featured an unpainted tank thus exposing the orange/rust colored foam insulation. This resulted in a weight saving of over 1,000 lb (450 kg), a savings that translated directly to added payload capacity to orbit. NASA's Space Shuttle, officially called Space Transportation System (STS), is the United States government's sole manned launch vehicle currently in service. The winged shuttle orbiter is launched vertically, carrying usually five to seven astronauts and up to about 22,700 kg (50,000 lbs) of payload into low earth orbit. When its mission is complete, it reenters the earth's atmosphere and makes an unpowered gliding horizontal landing, usually on a runway at Kennedy Space Center. The Space Shuttle orbiter was manufactured by North American Rockwell, now part of the Boeing Company. Martin Marietta (now part of Lockheed Martin) designed the external fuel tank and Morton Thiokol (now part of Alliant Techsystems (ATK)) designed the solid rocket boosters. The Shuttle is the first orbital spacecraft designed for partial reusability. It carries large payloads to various orbits, provides crew rotation for the International Space Station (ISS), and performs servicing missions. While the vehicle was designed with the capacity to recover satellites and other payloads from orbit and return them to Earth, this capacity has not been used often; it is, however, an important use of the Space Shuttle in the context of the ISS program, as only very small amounts of experimental material, hardware needing to be repaired, and trash can be returned by Soyuz. -
Developing the Space Shuttle1
****EU4 Chap 2 (161-192) 4/2/01 12:45 PM Page 161 Chapter Two Developing the Space Shuttle1 by Ray A. Williamson Early Concepts of a Reusable Launch Vehicle Spaceflight advocates have long dreamed of building reusable launchers because they offer relative operational simplicity and the potential of significantly reduced costs com- pared to expendable vehicles. However, they are also technologically much more difficult to achieve. German experimenters were the first to examine seriously what developing a reusable launch vehicle (RLV) might require. During the 1920s and 1930s, they argued the advantages and disadvantages of space transportation, but were far from having the technology to realize their dreams. Austrian engineer Eugen M. Sänger, for example, envi- sioned a rocket-powered bomber that would be launched from a rocket sled in Germany at a staging velocity of Mach 1.5. It would burn rocket fuel to propel it to Mach 10, then skip across the upper reaches of the atmosphere and drop a bomb on New York City. The high-flying vehicle would then continue to skip across the top of the atmosphere to land again near its takeoff point. This idea was never picked up by the German air force, but Sänger revived a civilian version of it after the war. In 1963, he proposed a two-stage vehi- cle in which a large aircraft booster would accelerate to supersonic speeds, carrying a rel- atively small RLV to high altitudes, where it would be launched into low-Earth orbit (LEO).2 Although his idea was advocated by Eurospace, the industrial consortium formed to promote the development of space activities, it was not seriously pursued until the mid- 1980s, when Dornier and other German companies began to explore the concept, only to drop it later as too expensive and technically risky.3 As Sänger’s concepts clearly illustrated, technological developments from several dif- ferent disciplines must converge to make an RLV feasible. -
Worldwide Equipment Guide
WORLDWIDE EQUIPMENT GUIDE TRADOC DCSINT Threat Support Directorate DISTRIBUTION RESTRICTION: Approved for public release; distribution unlimited. Worldwide Equipment Guide Sep 2001 TABLE OF CONTENTS Page Page Memorandum, 24 Sep 2001 ...................................... *i V-150................................................................. 2-12 Introduction ............................................................ *vii VTT-323 ......................................................... 2-12.1 Table: Units of Measure........................................... ix WZ 551........................................................... 2-12.2 Errata Notes................................................................ x YW 531A/531C/Type 63 Vehicle Series........... 2-13 Supplement Page Changes.................................... *xiii YW 531H/Type 85 Vehicle Series ................... 2-14 1. INFANTRY WEAPONS ................................... 1-1 Infantry Fighting Vehicles AMX-10P IFV................................................... 2-15 Small Arms BMD-1 Airborne Fighting Vehicle.................... 2-17 AK-74 5.45-mm Assault Rifle ............................. 1-3 BMD-3 Airborne Fighting Vehicle.................... 2-19 RPK-74 5.45-mm Light Machinegun................... 1-4 BMP-1 IFV..................................................... 2-20.1 AK-47 7.62-mm Assault Rifle .......................... 1-4.1 BMP-1P IFV...................................................... 2-21 Sniper Rifles..................................................... -
Lockheed-Martin OV-200 Class Space Shuttle (2011 –2138)
- 1 - Original texts and document concept copyright © 2007 by Richard E. Mandel STAR TREK, its on-screen derivatives, and all associated materials are the property of Paramount Pictures Corporation. Multiple references in this document are given under the terms of fair use with regard to international copyright and trademark law. This is a scholarly reference work intended to explain the background and historical aspects of STAR TREK and its spacecraft technology and is not sponsored, approved, or authorized by Paramount Pictures and its affiliated licensees. All visual materials included herein is protected by either implied or statutory copyright and are reproduced either with the permission of the copyright holder or under the terms of fair use as defined under current international copyright law. All visual materials used in this work without clearance were obtained from public sources through public means and were believed to be in the public domain or available for inclusion via the fair use doctrine at the time of printing. Cover art composited from the work of Andrew J. Hodges (DY-100) and Industrial Light and Magic (Excelsior) This work is dedicated to Geoffery Mandel, who started it for all of us. Memory Alpha and SFHQ/Mastercom cataloging data: UFP/SFD DTA HR:217622 - 2 - Gfefsbujpo!Tqbdfgmjhiu!Dispopmphz! First History (Prime Two) Edition Modified Okuda Timeline preview build 20070915 by Richard E. Mandel - 3 - Table of Contents Notes to self: no more than five major starships per section, ONLY canon/semi-canon/licensed/“reality” -
Round Trip to Orbit: Human Spaceflight Alternatives
Round Trip to Orbit: Human Spaceflight Alternatives August 1989 NTIS order #PB89-224661 Recommended Citation: U.S. Congress, Office of Technology Assessment, Round Trip to Orbit: Human Spaceflight Alternatives Special Report, OTA-ISC-419 (Washington, DC: U.S. Government Printing Office, August 1989). Library of Congress Catalog Card Number 89-600744 For sale by the Superintendent of Documents U.S. Government Printing Office, Washington, DC 20402-9325 (order form can be found in the back of this special report) Foreword In the 20 years since the first Apollo moon landing, the Nation has moved well beyond the Saturn 5 expendable launch vehicle that put men on the moon. First launched in 1981, the Space Shuttle, the world’s first partially reusable launch system, has made possible an array of space achievements, including the recovery and repair of ailing satellites, and shirtsleeve research in Spacelab. However, the tragic loss of the orbiter Challenger and its crew three and a half years ago reminded us that space travel also carries with it a high element of risk-both to spacecraft and to people. Continued human exploration and exploitation of space will depend on a fleet of versatile and reliable launch vehicles. As this special report points out, the United States can look forward to continued improvements in safety, reliability, and performance of the Shuttle system. Yet, early in the next century, the Nation will need a replacement for the Shuttle. To prepare for that eventuality, NASA and the Air Force have begun to explore the potential for advanced launch systems, such as the Advanced Manned Launch System and the National Aerospace Plane, which could revolutionize human access to space. -
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. -
Indigenous Peoples in the Russian Federation
INDIGENOUS PEOPLES IN THE RUSSIAN FEDERATION INDIGENOUS PEOPLES IN THE RUSSIAN FEDERATION Johannes Rohr Report 18 IWGIA – 2014 INDIGENOUS PEOPLES IN THE RUSSIAN FEDERATION Copyright: IWGIA Author: Johannes Rohr Editor: Diana Vinding and Kathrin Wessendorf Proofreading: Elaine Bolton Cover design and layout: Jorge Monrás Cover photo: Sakhalin: Indigenous ceremony opposite to oil facilities. Photographer: Wolfgang Blümel Prepress and print: Electronic copy only Hurridocs Cip data Title: IWGIA Report 18: Indigenous Peoples in the Russian Federation Author: Johannes Rohr Editor: Diana Vinding and Kathrin Wessendorf Number of pages: 69 ISBN: 978-87-92786-49-4 Language: English Index: 1. Indigenous peoples – 2. Human rights Geographical area: Russian Federation Date of publication: 2014 INTERNATIONAL WORK GROUP FOR INDIGENOUS AFFAIRS Classensgade 11 E, DK 2100 - Copenhagen, Denmark Tel: (45) 35 27 05 00 - Fax: (45) 35 27 05 07 E-mail: [email protected] - Web: www.iwgia.org This report has been prepared and published with the financial support of the Foreign Ministry of Denmark through its Neighbourhood programme. CONTENTS Introduction................................................................................................................................................................. 8 1 The indigenous peoples of the north ................................................................................................................... 9 1.1 Matters of definition ......................................................................................................................................... -
Waterbirds of Lake Baikal, Eastern Siberia, Russia
FORKTAIL 25 (2009): 13–70 Waterbirds of Lake Baikal, eastern Siberia, Russia JIŘÍ MLÍKOVSKÝ Lake Baikal lies in eastern Siberia, Russia. Due to its huge size, its waterbird fauna is still insufficiently known in spite of a long history of relevant research and the efforts of local and visiting ornithologists and birdwatchers. Overall, 137 waterbird species have been recorded at Lake Baikal since 1800, with records of five further species considered not acceptable, and one species recorded only prior to 1800. Only 50 species currently breed at Lake Baikal, while another 11 species bred there in the past or were recorded as occasional breeders. Only three species of conservation importance (all Near Threatened) currently breed or regularly migrate at Lake Baikal: Asian Dowitcher Limnodromus semipalmatus, Black-tailed Godwit Limosa limosa and Eurasian Curlew Numenius arquata. INTRODUCTION In the course of past centuries water levels in LB fluctuated considerably (Galaziy 1967, 1972), but the Lake Baikal (hereafter ‘LB’) is the largest lake in Siberia effects on the local avifauna have not been documented. and one of the largest in the world. Avifaunal lists of the Since the 1950s, the water level in LB has been regulated broader LB area have been published by Gagina (1958c, by the Irkutsk Dam. The resulting seasonal fluctuations 1960b,c, 1961, 1962b, 1965, 1968, 1988), Dorzhiyev of water levels significantly influence the distribution and (1990), Bold et al. (1991), Dorzhiyev and Yelayev (1999) breeding success of waterbirds (Skryabin 1965, 1967a, and Popov (2004b), but the waterbird fauna has not 1995b, Skryabin and Tolchin 1975, Lipin et al. -
Marks" Small Aviation-Rocket Space Launch System
Journal of Engineering Science and Technology Vol. 13, No. 5 (2018) 1143 - 1152 © School of Engineering, Taylor’s University "MARKS" SMALL AVIATION-ROCKET SPACE LAUNCH SYSTEM A. V. SMOLYAKOV*, V. A. YANAKAEV, A. V. KORNEV, S. V. SHEVKO "NII PFM KhAI" Research Institute, National Aerospace University "Kharkov Aviation Institute" named after N.Ye. Zhukovsky, No. 17, Chkalova str., 61070, Kharkov, Ukraine *Corresponding Author: [email protected] Abstract The problems of delivery of small space vehicles into low earth orbits are pointed out. The up-to-date means for the ascent of small space vehicles into low earth orbits are analysed. The solution for responsive and economical ascent of small space vehicles into low earth orbits in the form of "MARKS" small aviation- rocket space launch system is offered. Implementation of the offered idea will provide the price of delivery of 1 kg payload into 500 km sun-synchronous orbit equal to 3750 US dollars. Keywords: Small space vehicle, Low Earth orbit, Space launch vehicle, Aviation- rocket space launch system. 1. Introduction Owing to reduction of weight, overall dimensions, power consumption and costs of electronic components for space satellites, a number of proposals concerning delivery of small space vehicles (SSV) into low earth orbits (LEO) is promptly increased. At the same time in the world market of space launch services presented by various rocket space launch vehicles (SLV) and aviation-rocket space launch systems (ARSLS), practically there are no specialized, responsive and economical systems for SSV delivery into LEO. It is offered to solve the problem of responsive and economical ascent of SSV into LEO by means of creation of "MARKS" small modular ARSLS. -
The Chelomei Alternative to Buran
“LKS” The Chelomei alternative to Buran Giuseppe De Chiara 31 – 08 – 2012 All the drawings are copyright of the author Foreword In 1976 the Soviet government formally authorized the “head-designer” Valentin Glushko to proceed with the Buran project, intended as a mere Space Shuttle copy at that times in advanced development stage. The Buran project, and its massive launcher Energia (strongly supported by Glushko himself) were the targets of several critics among Russian space designers and scientists. One of them was the authored Vladimir Chelomei, a Glushko’s former alley, and also responsible of the famous OKB-52 (from which was sorted the Proton rocket, the TKS spacecraft and the Almaz and Salyut space stations). Chelomei affirmed that the Buran project was too big, heavy and expensive for the Russian possibilities of that times so he proposed, as alternative, a scaled down copy of the actual Space Shuttle, such spacecraft would be lighter and launched by one of his Proton rockets. The result of such idea was the LKS ( Легкий Космический Самолет – Light Spaceplane) project, proposed in 1979 as alternative to Buran/Energia. The LKS maintained all the main features of the original Shuttle/Buran project only scaled down, included a cargo bay with the possibility to carry a wide range of both military and civilian payloads to LEO. In 1980 Chelomei ordered the construction of a full scale mock-up that was realized by his team in only one month of full ahead work, as way to further stimulate Soviet authorities in his direction. In 1982 was officially ordered to stop Chelomei any further activity about the LKS project and was reprised to had expended more than 400.000 rubles in a program not formally authorized as the LKS was. -
REMEMBERING the SPACE AGE ISBN 978-0-16-081723-6 F Asro El Yb T Eh S Epu Ir Tn E Edn Tn Fo D Co Mu E Tn S , .U S
REMEMBERING the SPACE AGE ISBN 978-0-16-081723-6 F asro le b yt eh S epu ir tn e edn tn fo D co mu e tn s , .U S . G evo r emn tn irP tn i Ogn eciff I tn re en :t skoob t ro e .Popgenoh .vog : lot l f ree ( 0081 215 )-;668 DC a re a( 0081 215 )-202 90000 aF :x ( M4012 a215 )-202 :li S t Ipo DCC, W ihsa gn t no , D C 20402 - 1000 ISBN 978-0-16-081723-6 9 780160 817236 ISBN 978-0-16-081723-6 F ro as el b yt eh S pu e ir tn e dn e tn fo D co mu e tn s, .U S . G vo er mn e tn P ir tn i gn O eciff I tn re en :t koob s . ro t e opg . vog P noh e : lot l f eer ( 668 ) 215 - 0081 ; DC a er a ( 202 ) 215 - 0081 90000 aF :x ( 202 ) 215 - 4012 Ma :li S t po I DC ,C W a hs i gn t no , D C 20402 - 1000 ISBN 978-0-16-081723-6 9 780160 817236 REMEMBERING the SPACE AGE Steven J. Dick Editor National Aeronautics and Space Administration Office of External Relations History Division Washington, DC 2008 NASA SP-2008-4703 Library of Congress Cataloging-in-Publication Data Remembering the Space Age / Steven J. Dick, editor. p. cm. Includes bibliographical references. 1. Astronautics--History--20th century. I. Dick, Steven J. TL788.5.R46 2008 629.4’109045--dc22 2008019448 CONTENTS Acknowledgments .......................................vii Introduction .......................................... -
Abstract Keywords Abbreviations
A review of design issues specific to hypersonic flight vehicles (30/03/2016) D. Sziroczak, PhD, Cranfield University H. Smith, Professor, Cranfield University Abstract This paper provides an overview of the current technical issues and challenges associated with the design of hypersonic vehicles. Two distinct classes of vehicles are reviewed; Hypersonic Transports and Space Launchers, their common features and differences are examined. After a brief historical overview, the paper takes a multi- disciplinary approach to these vehicles, discusses various design aspects, and technical challenges. Operational issues are explored, including mission profiles, current and predicted markets, in addition to environmental effects and human factors. Technological issues are also reviewed, focusing on the three major challenge areas associated with these vehicles: aerothermodynamics, propulsion, and structures. In addition, matters of reliability and maintainability are also presented. The paper also reviews the certification and flight testing of these vehicles from a global perspective. Finally the current stakeholders in the field of hypersonic flight are presented, summarizing the active programs and promising concepts. Keywords Hypersonic Transport, Space Launcher, Design review Abbreviations AETB: Alumina Enhanced Thermal Barrier AFRSI: Advanced Flexible Reusable Surface Insulation AOA: Angle of Attack CFD: Computational Fluid Dynamics CG: Centre of Gravity EASA: European Aviation Safety Agency EMU: Extravehicular Mobility Unit ESA: