NSIAD-00-96R Space Station: Russian-Built and Service Module
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ORION ORION a to Z APOGEE to Break the Frangible Joints and Separate the Fairings, Three Parachutes
National Aeronautics and Space Administration ORION www.nasa.gov ORION A to Z APOGEE to break the frangible joints and separate the fairings, three parachutes. The next two parachutes will then VAN ALLEN RADIATION BELTS The term apogee refers to the point in an elliptical exposing the spacecraft to space. LAS - LAUNCH ABORT SYSTEM deploy and open. Once the spacecraft slows to around The Van Allen Belts are belts of plasma trapped by orbit when a spacecraft is farthest from the Earth. Orion’s Launch Abort System (LAS) is designed to 100 mph, the three main parachutes will then deploy the Earth’s magnetic field that shield the surface of During Exploration Flight Test-1, Orion’s flight path will GUPPY propel the crew module away from an emergency on using three pilot parachutes and slow the spacecraft the Earth from much of the radiation in space. During take it to an apogee of 3,600 miles. Just how high is The Super Guppy is a special airplane capable of the launch pad or during initial takeoff, moving the to around 20 mph for splashdown in the Pacific Ocean. Exploration Flight Test-1, Orion will pass within the Van that? A commercial airliner flies about 8 miles above transporting up to 26 tons in its cargo compartment crew away from danger. Orion’s LAS has three new When fully deployed, the canopies of three main Allen Radiation Belts and will spend more time in the the Earth’s surface, so Orion’s flight is 450 times farther measuring 25 feet tall, 25 feet wide, and 111 feet long. -
The Orbital-Hub: Low Cost Platform for Human Spaceflight After ISS
67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30 September 2016. Copyright ©2016 by the International Astronautical Federation (IAF). All rights reserved. IAC-16, B3,1,9,x32622 The Orbital-Hub: Low Cost Platform for Human Spaceflight after ISS O. Romberga, D. Quantiusa, C. Philpota, S. Jahnkea, W. Seboldta, H. Dittusb, S. Baerwaldeb, H. Schlegelc, M. Goldd, G. Zamkad, R. da Costae, I. Retate, R. Wohlgemuthe, M. Langee a German Aerospace Center (DLR), Institute of Space Systems, Bremen, Germany, [email protected] b German Aerospace Center (DLR), Executive Board, Space Research and Technology, Cologne, Germany, c European Space Agency (ESA) Contractor, Johnson Space Center, Houston, USA, d Bigelow Aerospace, Las Vegas / Washington, USA, e Airbus DS, Bremen, Germany Abstract The International Space Station ISS demonstrates long-term international cooperation between many partner governments as well as significant engineering and programmatic achievement mostly as a compromise of budget, politics, administration and technological feasibility. A paradigm shift to use the ISS more as an Earth observation platform and to more innovation and risk acceptance can be observed in the development of new markets by shifting responsibilities to private entities and broadening research disciplines, demanding faster access by users and including new launcher and experiment facilitator companies. A review of worldwide activities shows that all spacefaring nations are developing their individual programmes for the time after ISS. All partners are basically still interested in LEO and human spaceflight as discussed by the ISECG. ISS follow-on activities should comprise clear scientific and technological objectives combined with the long term view on space exploration. -
For Steady Production of H-II Transfer Vehicle“KOUNOTORI”Series,Mitsubishi Heavy Industries Technical Review Vol.50 No.1(20
Mitsubishi Heavy Industries Technical Review Vol. 50 No. 1 (March 2013) 68 For Assured Production of “KOUNOTORI” Series H-II Transfer Vehicle YOICHIRO MIKI*1 KOICHI MATSUYAMA*2 KAZUMI MASUDA*3 HIROSHI SASAKI*4 The H-II Transfer Vehicle (HTV) is an unmanned but man-rated designed resupply spacecraft developed by Japan as a means of transporting supplies to the International Space Station (ISS). Since the launch of vehicle No. 1 on September 11, 2009, the HTVs have accomplished their missions three times in a row up to vehicle No. 3 in July 2012. Mitsubishi Heavy Industries, Ltd. (MHI) is managing the production of the HTVs from vehicle No. 2 as the prime contractor, and we are planning to launch another four vehicles up to No. 7. Need for the HTVs is increasing after the retirement of the U.S. Space Shuttle. This paper introduces the efforts taken for the assured production in order to maintain the continued success of the HTVs. |1. Introduction The H-II Transfer Vehicles (HTVs) have consecutively accomplished the three missions of the No. 1 demonstration flight vehicle in September 2009, the No. 2 first operational flight vehicle in January 2011 and No. 3 in July 2012. As a result of the Request for Proposal (RFP) competition, Japan Aerospace Exploration Agency (JAXA), selected Mitsubishi Heavy Industries, Ltd. (MHI) as the prime contractor for production of the operational flight HTVs as of No. 2. Accordingly, HTV No. 2 and No. 3 were manufactured under MHI’s management, leading to success. A wide variety of cargos have been transported by the three HTVs, showing the high versatility of the vehicle. -
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 -
Space Rescue Ensuring the Safety of Manned Space¯Ight David J
Space Rescue Ensuring the Safety of Manned Space¯ight David J. Shayler Space Rescue Ensuring the Safety of Manned Spaceflight Published in association with Praxis Publishing Chichester, UK David J. Shayler Astronautical Historian Astro Info Service Halesowen West Midlands UK Front cover illustrations: (Main image) Early artist's impression of the land recovery of the Crew Exploration Vehicle. (Inset) Artist's impression of a launch abort test for the CEV under the Constellation Program. Back cover illustrations: (Left) Airborne drop test of a Crew Rescue Vehicle proposed for ISS. (Center) Water egress training for Shuttle astronauts. (Right) Beach abort test of a Launch Escape System. SPRINGER±PRAXIS BOOKS IN SPACE EXPLORATION SUBJECT ADVISORY EDITOR: John Mason, B.Sc., M.Sc., Ph.D. ISBN 978-0-387-69905-9 Springer Berlin Heidelberg New York Springer is part of Springer-Science + Business Media (springer.com) Library of Congress Control Number: 2008934752 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, 2009 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. -
The New American Space Age: a Progress Report on Human Spaceflight the New American Space Age: a Progress Report on Human Spaceflight the International Space
The New American Space Age: A PROGRESS REPORT ON HUMAN SpaCEFLIGHT The New American Space Age: A Progress Report on Human Spaceflight The International Space Station: the largest international scientific and engineering achievement in human history. The New American Space Age: A Progress Report on Human Spaceflight Lately, it seems the public cannot get enough of space! The recent hit movie “Gravity” not only won 7 Academy Awards – it was a runaway box office success, no doubt inspiring young future scientists, engineers and mathematicians just as “2001: A Space Odyssey” did more than 40 years ago. “Cosmos,” a PBS series on the origins of the universe from the 1980s, has been updated to include the latest discoveries – and funded by a major television network in primetime. And let’s not forget the terrific online videos of science experiments from former International Space Station Commander Chris Hadfield that were viewed by millions of people online. Clearly, the American public is eager to carry the torch of space exploration again. Thankfully, NASA and the space industry are building a host of new vehicles that will do just that. American industry is hard at work developing new commercial transportation services to suborbital altitudes and even low Earth orbit. NASA and the space industry are also building vehicles to take astronauts beyond low Earth orbit for the first time since the Apollo program. Meanwhile, in the U.S. National Lab on the space station, unprecedented research in zero-g is paving the way for Earth breakthroughs in genetics, gerontology, new vaccines and much more. -
America's Greatest Projects and Their Engineers - VII
America's Greatest Projects and Their Engineers - VII Course No: B05-005 Credit: 5 PDH Dominic Perrotta, P.E. Continuing Education and Development, Inc. 22 Stonewall Court Woodcliff Lake, NJ 076 77 P: (877) 322-5800 [email protected] America’s Greatest Projects & Their Engineers-Vol. VII The Apollo Project-Part 1 Preparing for Space Travel to the Moon Table of Contents I. Tragedy and Death Before the First Apollo Flight A. The Three Lives that Were Lost B. Investigation, Findings & Recommendations II. Beginning of the Man on the Moon Concept A. Plans to Land on the Moon B. Design Considerations and Decisions 1. Rockets – Launch Vehicles 2. Command/Service Module 3. Lunar Module III. NASA’s Objectives A. Unmanned Missions B. Manned Missions IV. Early Missions V. Apollo 7 Ready – First Manned Apollo Mission VI. Apollo 8 - Orbiting the Moon 1 I. Tragedy and Death Before the First Apollo Flight Everything seemed to be going well for the Apollo Project, the third in a series of space projects by the United States intended to place an American astronaut on the Moon before the end of the 1960’s decade. Apollo 1, known at that time as AS (Apollo Saturn)-204 would be the first manned spaceflight of the Apollo program, and would launch a few months after the flight of Gemini 12, which had occurred on 11 November 1966. Although Gemini 12 was a short duration flight, Pilot Buzz Aldrin had performed three extensive EVA’s (Extra Vehicular Activities), proving that Astronauts could work for long periods of time outside the spacecraft. -
International Space Station Basics Components of The
National Aeronautics and Space Administration International Space Station Basics The International Space Station (ISS) is the largest orbiting can see 16 sunrises and 16 sunsets each day! During the laboratory ever built. It is an international, technological, daylight periods, temperatures reach 200 ºC, while and political achievement. The five international partners temperatures during the night periods drop to -200 ºC. include the space agencies of the United States, Canada, The view of Earth from the ISS reveals part of the planet, Russia, Europe, and Japan. not the whole planet. In fact, astronauts can see much of the North American continent when they pass over the The first parts of the ISS were sent and assembled in orbit United States. To see pictures of Earth from the ISS, visit in 1998. Since the year 2000, the ISS has had crews living http://eol.jsc.nasa.gov/sseop/clickmap/. continuously on board. Building the ISS is like living in a house while constructing it at the same time. Building and sustaining the ISS requires 80 launches on several kinds of rockets over a 12-year period. The assembly of the ISS Components of the ISS will continue through 2010, when the Space Shuttle is retired from service. The components of the ISS include shapes like canisters, spheres, triangles, beams, and wide, flat panels. The When fully complete, the ISS will weigh about 420,000 modules are shaped like canisters and spheres. These are kilograms (925,000 pounds). This is equivalent to more areas where the astronauts live and work. On Earth, car- than 330 automobiles. -
International Space Station Overview
NASA Facts National Aeronautics and Space Administration Lyndon B. Johnson Space Center IS-1999-06-ISS022 Houston, Texas 77058 International Space Station June 1999 The International Space Station: An Overview The International Space Station is the largest and most complex international scientific project in history. The station represents a move of unprecedented scale off the home planet that began in 1998 with the launch of the first two components, the Unity and Zarya modules. Led by the United States, the International Space Station draws upon the scientific and technological resources of 16 nations: Canada, Japan, Russia, 11 nations of the European Space Agency and Brazil. More than four times as large as the Russian Mir space station, the completed International Space Station will have a mass of about 1 million pounds. It will measure about 360 feet across and 290 feet long, with almost an acre of solar panels to provide electrical power to six state-of-the-art laboratories. The first two station modules, the Russian-launched Zarya control module and U.S.-launched Unity connecting module, were assembled in orbit in late 1998. The station is in an orbit with an altitude of 250 statute miles with an inclination of 51.6 degrees. This orbit allows the station to be reached by the launch vehicles of all the international partners to provide a robust capability for the delivery of crews and supplies. The orbit also provides excellent Earth observations with coverage of 85 percent of the globe and over flight Artist's concept of the completed International Space Station of 95 percent of the population. -
Japan's Technical Prowess International Cooperation
Japan Aerospace Exploration Agency April 2016 No. 10 Special Features Japan’s Technical Prowess Technical excellence and team spirit are manifested in such activities as the space station capture of the HTV5 spacecraft, development of the H3 Launch Vehicle, and reduction of sonic boom in supersonic transport International Cooperation JAXA plays a central role in international society and contributes through diverse joint programs, including planetary exploration, and the utilization of Earth observation satellites in the environmental and disaster management fields Japan’s Technical Prowess Contents No. 10 Japan Aerospace Exploration Agency Special Feature 1: Japan’s Technical Prowess 1−3 Welcome to JAXA TODAY Activities of “Team Japan” Connecting the Earth and Space The Japan Aerospace Exploration Agency (JAXA) is positioned as We review some of the activities of “Team the pivotal organization supporting the Japanese government’s Japan,” including the successful capture of H-II Transfer Vehicle 5 (HTV5), which brought overall space development and utilization program with world- together JAXA, NASA and the International Space Station (ISS). leading technology. JAXA undertakes a full spectrum of activities, from basic research through development and utilization. 4–7 In 2013, to coincide with the 10th anniversary of its estab- 2020: The H3 Launch Vehicle Vision JAXA is currently pursuing the development lishment, JAXA defined its management philosophy as “utilizing of the H3 Launch Vehicle, which is expected space and the sky to achieve a safe and affluent society” and to become the backbone of Japan’s space development program and build strong adopted the new corporate slogan “Explore to Realize.” Under- international competitiveness. -
CRS Issue Brief for Congress Received Through the CRS Web
Order Code IB93017 CRS Issue Brief for Congress Received through the CRS Web Space Stations Updated December 8, 2003 Marcia S. Smith Resources, Science, and Industry Division Congressional Research Service ˜ The Library of Congress CONTENTS SUMMARY MOST RECENT DEVELOPMENTS BACKGROUND AND ANALYSIS Introduction The Space Station Program: 1984-1993 Space Station Freedom 1993 Redesign — the Clinton Administration Restructuring The International Space Station (ISS): 1993-Present ISS Design, Cost, Schedule, and Lifetime September 1993-January 2001: the Clinton Administration Cost Growth Cost Caps 2001-Present: the Bush Administration Cost Growth “Core Complete” Configuration Current Assembly Sequence The IMCE (“Young”) Task Force Concerns of the Non-U.S. Partners and U.S. Researchers The ReMaP and NRC Reports on ISS Scientific Research Orbital Space Plane (OSP): Crew Return/Crew Transfer Vehicle Risks and Benefits of Russian Participation, and the Iran Nonproliferation Act (INA) Congressional Action FY2003 FY2004 International Partners The Original Partners: Europe, Canada, and Japan Russia Issues For Congressional Consideration Impact of the Loss of Space Shuttle Columbia Cost and Cost Effectiveness Operations and Commercialization Issues Issues Related to Russia’s Participation LEGISLATION IB93017 12-08-03 Space Stations SUMMARY Congress continues to debate NASA’s bring Russia into the program was a dramatic International Space Station (ISS) program to change. Under the 1993 agreement, Phase I of build a permanently occupied space station in U.S./Russian space station cooperation in- Earth orbit where astronauts live and conduct volved flights of Russians on the U.S. space research. NASA expects that research per- shuttle and Americans on Russia’s Mir space formed in the near-zero gravity environment station. -
CSM15 Launch Escape System
LAUNCH ESCAPE PITCH CONTROL MOTO TOWER JETTISON MOTOR LAUNCH ESCAPE MOTO CANARD LAUNCH ESCAPE MOTOR ACTUATOR THRUST ALIGNMENT FITIING STU OS & POWER SYSTEMS & INSTRUMENTATION WIRE HARNESS FRANGIBLE LAUNCH ESCAPE TOWER ELECTRICAL DISCONNECT FITIINGS P-186 BOOST PROTECTIVE COVER (APEX SECTION) Launch escape subsystem The launch escape subsystem will take the com nozzles and at the bottom to the command module mand module containing the astronauts away from by means of an explosive connection. the launch vehicle in case of an emergency on the pad or shortly after launch. The subsystem carries A boost protective cover is attached to the tower the CM to a sufficient height and to the side, away and completely covers the command module. This from the launch vehicle, so that the earth landing cover protects the command module from the subsystem can operate. rocket exhaust and also from the heating generated by launch vehicle boost through the atmosphere. It The subsystem looks like a large rocket con remains attached to the tower and is carried away nected to the command module by a lattice-work when the launch escape assembly is jettisoned. tower. It is 33 feet long and weighs about 8,000 pounds. The maximum diameter of the launch The subsystem is activated automatically by the escape assembly is four feet. emergency detection system in the first 100 seconds or manually by the astronauts at any time The forward or rocket section of the subsystem from the pad to jettison altitude. With the Saturn is cylindrical and houses three solid-propellant V, the subsystem is jettisoned at about 295,000 rocket motors and a ballast compartment topped by feet, or about 30 seconds after ignition of the a nose cone containing instruments.