“ESPI BRIEFS” No. 18
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Bibliography Books and reports Blandford, R.D. (Chair) New Worlds, New Horizons in Astronomy and Astrophysics Committee for a Decadal Survey of Astronomy and Astrophysics, National Research Council, 2010 Bondi, Hermann. et al Pioneering in Outer Space Heinemann Educational Books, 1971 Clarke, Arthur C. The Exploration of Space Temple Press, London, 1951 Department of Energy/NASA Satellite Power Systems Concept Development and Evaluation Program. DoE/NASA, October 1978 http://www.nss.org/settlement/ssp/library/1978DOESPS-ReferenceSystemReport.pdf Satellite Power Systems (SPS) Space Transportation Cost Analysis and Evaluation. DoE/NASA, November 1980 http://www.nss.org/settlement/ssp/library/1980DOESPS- SpaceTransportationCostAnalysis.pdf Dick, Steven J. (editor) Remembering the Space Age: Proceedings of the 50th Anniversary Conference. NASA SP-2008-4703, 2008 http://history.nasa.gov/Remembering_Space_Age_A.pdf © Springer International Publishing AG 2017 235 M. van Pelt, Dream Missions, Springer Praxis Books, DOI 10.1007/978-3-319-53941-6 236 Bibliography Dyson, George Project Orion: The True Story of the Atomic Spaceship Henry Holt & Company, Inc., USA, 2002 Ehricke, Krafft A. Solar Transportation In Space Age in Fiscal Year 2001, Proceedings of the Fourth AAS Goddard Memorial Symposium American Astronautical Society, 1966 Friedman, Louis. Human Spaceflight, from Mars to the Stars The University of Arizona Press, 2015 Gatland, Kenneth W. & Bono, Philip Frontiers of Space Blandford Press, UK, 1969 Hansen, James R. Chapter 9, Skipping “The Next Logical Step” in Spaceflight Revolution; NASA Langley Research Center from Sputnik to Apollo NASA History Series SP-4308, USA, 1994 http://history.nasa.gov/SP-4308/ch9.htm Koelle, Heinz-Hermann. Nova and Beyond, a Review of Heavy Lift Launch Vehicle Concepts in the Post-Saturn Class Technical University Berlin, Germany, 2001 Konecci, Eugene B. -
Space Launch System (Sls) Motors
Propulsion Products Catalog SPACE LAUNCH SYSTEM (SLS) MOTORS For NASA’s Space Launch System (SLS), Northrop Grumman manufactures the five-segment SLS heavy- lift boosters, the booster separation motors (BSM), and the Launch Abort System’s (LAS) launch abort motor and attitude control motor. The SLS five-segment booster is the largest solid rocket motor ever built for flight. The SLS booster shares some design heritage with flight-proven four-segment space shuttle reusable solid rocket motors (RSRM), but generates 20 percent greater average thrust and 24 percent greater total impulse. While space shuttle RSRM production has ended, sustained booster production for SLS helps provide cost savings and access to reliable material sources. Designed to push the spent RSRMs safely away from the space shuttle, Northrop Grumman BSMs were rigorously qualified for human space flight and successfully used on the last fifteen space shuttle missions. These same motors are a critical part of NASA’s SLS. Four BSMs are installed in the forward frustum of each five-segment booster and four are installed in the aft skirt, for a total of 16 BSMs per launch. The launch abort motor is an integral part of NASA’s LAS. The LAS is designed to safely pull the Orion crew module away from the SLS launch vehicle in the event of an emergency on the launch pad or during ascent. Northrop Grumman is on contract to Lockheed Martin to build the abort motor and attitude control motor—Lockheed is the prime contractor for building the Orion Multi-Purpose Crew Vehicle designed for use on NASA’s SLS. -
Paper Session IA-Shuttle-C Heavy-Lift Vehicle of the 90'S
The Space Congress® Proceedings 1989 (26th) Space - The New Generation Apr 25th, 2:00 PM Paper Session I-A - Shuttle-C Heavy-Lift Vehicle of the 90's Robert G. Eudy Manager, Shuttle-C Task Team, Marshall Space Flight Center Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Eudy, Robert G., "Paper Session I-A - Shuttle-C Heavy-Lift Vehicle of the 90's" (1989). The Space Congress® Proceedings. 5. https://commons.erau.edu/space-congress-proceedings/proceedings-1989-26th/april-25-1989/5 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. SHUTTLE-C HEAVY-LIFT VEHICLE OF THE 90 ' S Mr. Robert G. Eudy, Manager Shuttle-C Task Team Marshall Space Flight Center ABSTRACT United States current and planned space activities identify the need for increased payload capacity and unmanned flight to complement the existing Shuttle. To meet this challenge the National Aeronautics and Space Administration is defining an unmanned cargo version of the Shuttle that can give the nation early heavy-lift capability. Called Shuttle-C, this unmanned vehicle is a natural, low-cost evolution of the current Space Shuttle that can be flying 100,000 to 170,000 pound payloads by late 1994. At the core of Shuttle-C design philosophy is the principle of evolvement from the United State's Space Transportation System. -
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www.arianespace.com www.starsem.com www.avio Arianespace’s eighth launch of 2021 with the fifth Soyuz of the year will place its satellite passengers into low Earth orbit. The launcher will be carrying a total payload of approximately 5 518 kg. The launch will be performed from Baikonur, in Kazakhstan. MISSION DESCRIPTION 2 ONEWEB SATELLITES 3 Liftoff is planned on at exactly: SOYUZ LAUNCHER 4 06:23 p.m. Washington, D.C. time, 10:23 p.m. Universal time (UTC), LAUNCH CAMPAIGN 4 00:23 a.m. Paris time, FLIGHT SEQUENCES 5 01:23 a.m. Moscow time, 03:23 a.m. Baikonur Cosmodrome. STAKEHOLDERS OF A LAUNCH 6 The nominal duration of the mission (from liftoff to separation of the satellites) is: 3 hours and 45 minutes. Satellites: OneWeb satellite #255 to #288 Customer: OneWeb • Altitude at separation: 450 km Cyrielle BOUJU • Inclination: 84.7degrees [email protected] +33 (0)6 32 65 97 48 RUAG Space AB (Linköping, Sweden) is the prime contractor in charge of development and production of the dispenser system used on Flight ST34. It will carry the satellites during their flight to low Earth orbit and then release them into space. The dedicated dispenser is designed to Flight ST34, the 29th commercial mission from the Baikonur Cosmodrome in Kazakhstan performed by accommodate up to 36 spacecraft per launch, allowing Arianespace and its Starsem affiliate, will put 34 of OneWeb’s satellites bringing the total fleet to 288 satellites Arianespace to timely deliver the lion’s share of the initial into a near-polar orbit at an altitude of 450 kilometers. -
Incredible Results in IAS 2013 5 Ranks 62 Ranks in Top 50 Ranks in the Final List
RESULTS Incredible results in IAS 2013 5 Ranks 62 Ranks in Top 50 Ranks in the final list Rank 9 Rank 12 Rank 23 Rank 40 Rank 46 Divyanshu Jha Neha Jain Prabhav joshi Gaurang Rathi Udita Singh We broke our past record in IAS 2014 6 Ranks 12 Ranks 83 Ranks in Top 50 in Top 100 Overall Selections Rank 4 Rank 5 Rank 16 Rank 23 Rank 28 Rank 39 Vandana Rao Suharsha Bhagat Ananya Das Anil Dhameliya Kushaal Yadav Vivekanand T.S We did it again in IAS 2015 5 Ranks 14 Ranks 162 Ranks in Top 50 in Top 100 In The Final List Rank 20 Rank 24 Rank 25 Rank 27 Rank 47 Vipin Garg Khumanthem Chandra Pulkit Garg Anshul Diana Devi Mohan Garg Agarwal And we’ve done it yet again in IAS 2016 8 Ranks 18 Ranks 215 Ranks in Top 50 in Top 100 In The Final List Rank 2 Rank 5 Rank 12 Rank 30 Rank 32 Anmol Sher Abhilash Tejaswi Prabhash Avdhesh Singh Bedi Mishra Rana Kumar Meena And we’ve done it yet again in IAS 2017 5 Ranks 34 Ranks 236 Ranks in Top 10 in Top 100 In The Final List Rank 3 Rank 6 Rank 8 Rank 9 Rank 10 Sachin Koya sree Anubhav Saumya Abhishek Gupta Harsha Singh Sharma Surana Ashima Abhijeet Varjeet Keerthi Utsav Gaurav Abhilash Vikramaditya Vishal Mittal Sinha Walia Vasan V Gautam Kumar Baranwal Singh Malik Mishra Rank-12 Rank-19 Rank-21 Rank-29 Rank-33 Rank-34 Rank-44 Rank-48 Rank-49 Sambit Bodke Akshat Jagdish Hirani Swapneel Jyoti Pushp Amol Mishra Digvijay Govind Kaushal Chelani Adityavikram Paul Sharma Lata Srivastava Rank-51 Rank-54 Rank-55 Rank-57 Rank-60 Rank-64 Rank-75 Rank-80 Rank-83 Prateek Amilineni Sangh Rahul Kathawate Vaibhava Videh Plash -
Spaceport Infrastructure Cost Trends
AIAA 2014-4397 SPACE Conferences & Exposition 4-7 August 2014, San Diego, CA AIAA SPACE 2014 Conference and Exposition Spaceport Infrastructure Cost Trends Brian S. Gulliver, PE1, and G. Wayne Finger, PhD, PE2 RS&H, Inc. The total cost of employing a new or revised space launch system is critical to understanding its business potential, analyzing its business case and funding its development. The design, construction and activation of a commercial launch complex or spaceport can represent a significant portion of the non-recurring costs for a new launch system. While the historical cost trends for traditional launch site infrastructure are fairly well understood, significant changes in the approach to commercial launch systems in recent years have required a reevaluation of the cost of ground infrastructure. By understanding the factors which drive these costs, informed decisions can be made early in a program to give the business case the best chance of economic success. The authors have designed several NASA, military, commercial and private launch complexes and supported the evaluation and licensing of commercial aerospaceports. Data from these designs has been used to identify the major factors which, on a broad scale, drive their non-recurring costs. Both vehicle specific and location specific factors play major roles in establishing costs. I. Introduction It is critical for launch vehicle operators and other stakeholders to understand the factors and trends that affect the non-recurring costs of launch site infrastructure. These costs are often an area of concern when planning for the development of a new launch vehicle program as they can represent a significant capital investment that must be recovered over the lifecycle of the program. -
Launcherone Success Opens New Space Access Gateway Guy Norris January 22, 2021
1/22/21 7:05 1/6 LauncherOne Success Opens New Space Access Gateway Guy Norris January 22, 2021 With San Nicolas Island far below, LauncherOne headed for polar orbit. Credit: Virgin Orbit Virgin Orbit had barely tweeted news of the successful Jan. 17 space debut of its LauncherOne vehicle on social media when new launch contracts began arriving in the company’s email inbox. A testament to the pent-up market demand for small-satellite launch capability, the speedy reaction to the long-awaited demonstration of the new space-access vehicle paves the way for multiple follow-on Virgin Orbit missions by year-end and a potential doubling of the rate in 2022. First successful privately developed air-launched, liquid-fueled rocket Payloads deployed for NASA’s Venture Class Launch Services program The glitch-free !ight of LauncherOne on its second demonstration test was a critical and much-welcomed milestone for the Long Beach, California-based company. Coming almost nine years a"er the air-launch concept was #rst unveiled by Virgin founder Richard Branson, and six years a"er the start of full-scale development, the !ight followed last May’s #rst demonstration mission, which ended abruptly when the rocket motor shut o$ a"er just 4 sec. 1/22/21 7:05 2/6 A"er an exhaustive analysis and modi#cations to beef up the oxidizer feed line at the heart of the #rst !ight failure, the path to the Launch Demo 2 test was then delayed until January 2021 by the COVID-19 pandemic. With the LauncherOne system now proven, design changes veri#ed and the #rst 10 small satellites placed in orbit, Virgin Orbit is already focusing on the next steps to ramp up its production and launch-cadence capabilities. -
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. -
IAF SPACE TRANSPORTATION SOLUTIONS and INNOVATIONS SYMPOSIUM (D2) Small Launchers: Concepts and Operations (Part I) (7)
69th International Astronautical Congress 2018 Paper ID: 44054 oral IAF SPACE TRANSPORTATION SOLUTIONS AND INNOVATIONS SYMPOSIUM (D2) Small Launchers: Concepts and Operations (Part I) (7) Author: Ms. Sirisha Bandla Virgin Galactic L.L.C, United States, [email protected] Ms. Monica Jan Virgin Galactic L.L.C, United States, [email protected] LAUNCHERONE: RESPONSIVE LAUNCH FOR SMALL SATELLITES Abstract Virgin Orbit is a developing small launch platform that will provide affordable, dedicated rides to orbit for small satellites starting this year. We are in the midst of a small satellite revolution and with technology advancement packing more capability in smaller packages, small satellites are progressively pro- viding solutions for remote sensing, communications, earth observation and other low-Earth orbit needs. Currently, a small satellite operator is typically forced to ride as a secondary payload, constrained to the primary payload's launch schedule and orbit. However, Virgin Orbit's small launch vehicle, LauncherOne, will soon begin providing frequent, affordable, and dedicated transportation to orbit for small payloads. LauncherOne is a two stage, liquid propulsion (LOX/RP) rocket launched from a Boeing 747-400. By utilizing air-launch, the system is designed to conduct operations from a variety of locations, removing the complexity and scheduling typically associated with traditional launch ranges. LauncherOne will allow customers to select from various launch azimuths, including equatorial inclinations, and will increase avail- able orbital launch windows. The Long Beach, California, USA facility where the team is based has been outfitted with the equipment needed for the manufacture of the LauncherOne rocket, and currently staffs over 300 employees. -
The European Launchers Between Commerce and Geopolitics
The European Launchers between Commerce and Geopolitics Report 56 March 2016 Marco Aliberti Matteo Tugnoli Short title: ESPI Report 56 ISSN: 2218-0931 (print), 2076-6688 (online) Published in March 2016 Editor and publisher: European Space Policy Institute, ESPI Schwarzenbergplatz 6 • 1030 Vienna • Austria http://www.espi.or.at Tel. +43 1 7181118-0; Fax -99 Rights reserved – No part of this report may be reproduced or transmitted in any form or for any purpose with- out permission from ESPI. Citations and extracts to be published by other means are subject to mentioning “Source: ESPI Report 56; March 2016. All rights reserved” and sample transmission to ESPI before publishing. ESPI is not responsible for any losses, injury or damage caused to any person or property (including under contract, by negligence, product liability or otherwise) whether they may be direct or indirect, special, inciden- tal or consequential, resulting from the information contained in this publication. Design: Panthera.cc ESPI Report 56 2 March 2016 The European Launchers between Commerce and Geopolitics Table of Contents Executive Summary 5 1. Introduction 10 1.1 Access to Space at the Nexus of Commerce and Geopolitics 10 1.2 Objectives of the Report 12 1.3 Methodology and Structure 12 2. Access to Space in Europe 14 2.1 European Launchers: from Political Autonomy to Market Dominance 14 2.1.1 The Quest for European Independent Access to Space 14 2.1.3 European Launchers: the Current Family 16 2.1.3 The Working System: Launcher Strategy, Development and Exploitation 19 2.2 Preparing for the Future: the 2014 ESA Ministerial Council 22 2.2.1 The Path to the Ministerial 22 2.2.2 A Look at Europe’s Future Launchers and Infrastructure 26 2.2.3 A Revolution in Governance 30 3. -
Please Type Your Paper Title Here In
Estimating the Reliability of a Soyuz Spacecraft Mission Michael G. Lutomskia*, Steven J. Farnham IIb, and Warren C. Grantb aNASA-JSC, Houston, TX – [email protected] bARES Corporation, Houston, TX Abstract: Once the US Space Shuttle retires in 2010, the Russian Soyuz Launcher and Soyuz Spacecraft will comprise the only means for crew transportation to and from the International Space Station (ISS). The U.S. Government and NASA have contracted for crew transportation services to the ISS with Russia. The resulting implications for the US space program including issues such as astronaut safety must be carefully considered. Are the astronauts and cosmonauts safer on the Soyuz than the Space Shuttle system? Is the Soyuz launch system more robust than the Space Shuttle? Is it safer to continue to fly the 30 year old Shuttle fleet for crew transportation and cargo resupply than the Soyuz? Should we extend the life of the Shuttle Program? How does the development of the Orion/Ares crew transportation system affect these decisions? The Soyuz launcher has been in operation for over 40 years. There have been only two loss of life incidents and two loss of mission incidents. Given that the most recent incident took place in 1983, how do we determine current reliability of the system? Do failures of unmanned Soyuz rockets impact the reliability of the currently operational man-rated launcher? Does the Soyuz exhibit characteristics that demonstrate reliability growth and how would that be reflected in future estimates of success? NASA’s next manned rocket and spacecraft development project is currently underway. -
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.