Rocket Launchers for Small Satellites Ajey Lele and Tushar Shrivastav
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“Where Do I Start?” Rides to Space for Scientific and Academic Payloads
SSC02-VII-06 “WHERE DO I START?” RIDES TO SPACE FOR SCIENTIFIC AND ACADEMIC PAYLOADS Matt Bille Tony Williams Tracy Martin Booz, Allen & Hamilton Booz, Allen & Hamilton Booz, Allen & Hamilton 1050 S. Academy Blvd. #148 1050 S. Academy Blvd. #148 1050 S. Academy Blvd. #148 Colorado Springs, CO 80910 Colorado Springs, CO 80910 Colorado Springs, CO 80910 719-570-3172 719-570-3109 719-570-3105 [email protected] [email protected] [email protected] ABSTRACT. The launch problem for small payloads is nowhere as serious as it is for scientific and academic users, who cannot tap the purchasing power available to spacecraft funded by the military and large corporations. The options available for the researcher at a university who has an instrument or a spacecraft are limited, sometimes depressingly so. Dedicated vehicles are usually unaffordable, and secondary payload opportunities require meeting a host of requirements, from payload design to timing to integration, dependent on the needs of the primary payload. In this paper, the authors survey the options available and answer the question, “Where do I start?” Sources of potential rides, including NASA, military, commercial, and non-U.S. programs and organizations were surveyed. The results are presented here, along with recommendations for an improved process which, at low cost, could improve the “matchmaking” system and simplify the obstacle course faced by spacecraft and instrument developers today. Introduction Who To Call First While the technology to reduce the size and The payload developer can start by approaching increase the capability of small scientific and two government programs which aim to help in academic satellites continues to advance, the providing rides to space. -
In Flight Research on Aerothermodynamics (Atd) and Thermal Protection Systems (Tps) for Space Transportation Systems
1 IN FLIGHT RESEARCH ON AEROTHERMODYNAMICS (ATD) AND THERMAL PROTECTION SYSTEMS (TPS) FOR SPACE TRANSPORTATION SYSTEMS Jean Muylaert (1) , M. Ivanov (2) ,V. A. Danilkin (2), C. Park (3), H. Ritter (1), G. Ortega (1) (1)ESA/ESTEC, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands, Email: [email protected], [email protected], [email protected] (2) ITAM Email : [email protected] (3) SRC-MDB Email: [email protected] (4) KAIST Email:CPark216 @kaist.ac.kr ABSTRACT The paper addresses a strategy to perform in flight such as wake closure, capsule shoulder heating and TPS gap / step micro aero effects could be analysed. research on Aerothermodynamics (ATD) and Thermal Protection Systems (TPS) taking advantage of the low 4. Aero-assist Hopping being a General Study cost VOLNA and SHTIL class of launchers. Programme (GSP) internal activity to assess the A series of flight test beds will be addressed and their feasibility of a low cost flight gathering data on aero- relevance discussed as to the gathering of critical braking and aero-assist strategies. Aerothermodynamic and TPS related data for design It is concluded that these low cost class of in flight tool qualification and associated physical model research initiatives are “the” way forwards to improve validation. the tools to be used for design of future re-entry space transportation systems. The paper reviews 4 initiatives, all of them of the class flying test beds and launched by the VOLNA launcher: 1. BACKGROUND 1. The EXPERT (European Experimental re-entry Test bed) project where the objective is to acquire hypersonic The design of space transportation systems is always flight data for improved understanding of natural and driven by worst case scenario’s involving estimations of roughness induced boundary layer transition, catalysis uncertainties associated with critical phenomena. -
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. -
Redalyc.Status and Trends of Smallsats and Their Launch Vehicles
Journal of Aerospace Technology and Management ISSN: 1984-9648 [email protected] Instituto de Aeronáutica e Espaço Brasil Wekerle, Timo; Bezerra Pessoa Filho, José; Vergueiro Loures da Costa, Luís Eduardo; Gonzaga Trabasso, Luís Status and Trends of Smallsats and Their Launch Vehicles — An Up-to-date Review Journal of Aerospace Technology and Management, vol. 9, núm. 3, julio-septiembre, 2017, pp. 269-286 Instituto de Aeronáutica e Espaço São Paulo, Brasil Available in: http://www.redalyc.org/articulo.oa?id=309452133001 How to cite Complete issue Scientific Information System More information about this article Network of Scientific Journals from Latin America, the Caribbean, Spain and Portugal Journal's homepage in redalyc.org Non-profit academic project, developed under the open access initiative doi: 10.5028/jatm.v9i3.853 Status and Trends of Smallsats and Their Launch Vehicles — An Up-to-date Review Timo Wekerle1, José Bezerra Pessoa Filho2, Luís Eduardo Vergueiro Loures da Costa1, Luís Gonzaga Trabasso1 ABSTRACT: This paper presents an analysis of the scenario of small satellites and its correspondent launch vehicles. The INTRODUCTION miniaturization of electronics, together with reliability and performance increase as well as reduction of cost, have During the past 30 years, electronic devices have experienced allowed the use of commercials-off-the-shelf in the space industry, fostering the Smallsat use. An analysis of the enormous advancements in terms of performance, reliability and launched Smallsats during the last 20 years is accomplished lower prices. In the mid-80s, a USD 36 million supercomputer and the main factors for the Smallsat (r)evolution, outlined. -
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 . -
Beyond the United Kingdom: Trends in the Other Nuclear Armed States
Beyond the United Kingdom: Trends in the Other Nuclear Armed States Ian Kearns Discussion Paper 1 of the BASIC Trident Commission An independent, cross-party commission to examine UK nuclear weapons policy Published by British American Security Information Council (BASIC) November 2011 BASIC in London BASIC in Washington The Grayston Centre 110 Maryland Avenue NE 28 Charles Square Suite 205 London N1 6HT Washington DC 20002 Tel: +44 (0) 207 324 4680 Tel: +1 (0) 202 546 8055 Acknowledgements Author BASIC and the BASIC Trident Commission are grateful to Dr Ian Kearns is the Chief Executive of the European the Ploughshares Fund, the Joseph Rowntree Charitable Trust, Leadership Network (ELN), a member of the BASIC Trident the Polden Puckham Charitable Trust and the Nuclear Commission, and works as a consultant to the Commission Information Trust for their financial support of the work of and to RUSI on nuclear issues. Previously Ian was Acting the Commission. We would also like to thank all those who Director and Deputy Director of the Institute for Public have contributed to the work of the Commission by Policy Research (IPPR) in the United Kingdom and Deputy submitting evidence and otherwise engaging in our activities. Chair of the IPPR’s independent All-Party Commission on National Security in the 21st Century, serving under co-chairs, BASIC would also like to thank the BASIC Trident Lord George Robertson and Lord Paddy Ashdown. He also Commissioners for their unpaid involvement in this enterprise. served in 2010 as a Specialist Adviser to the Joint House of Commons/House of Lords Committee on National Security. -
Russia Missile Chronology
Russia Missile Chronology 2007-2000 NPO MASHINOSTROYENIYA | KBM | MAKEYEV DESIGN BUREAU | MITT | ZLATOUST MACHINE-BUILDING PLANT KHRUNICHEV | STRELA PRODUCTION ASSOCIATION | AAK PROGRESS | DMZ | NOVATOR | TsSKB-PROGRESS MKB RADUGA | ENERGOMASH | ISAYEV KB KHIMMASH | PLESETSK TEST SITE | SVOBODNYY COSMODROME 1999-1996 KRASNOYARSK MACHINE-BUILDING PLANT | MAKEYEV DESIGN BUREAU | MITT | AAK PROGRESS NOVATOR | SVOBODNYY COSMODROME Last update: March 2009 This annotated chronology is based on the data sources that follow each entry. Public sources often provide conflicting information on classified military programs. In some cases we are unable to resolve these discrepancies, in others we have deliberately refrained from doing so to highlight the potential influence of false or misleading information as it appeared over time. In many cases, we are unable to independently verify claims. Hence in reviewing this chronology, readers should take into account the credibility of the sources employed here. Inclusion in this chronology does not necessarily indicate that a particular development is of direct or indirect proliferation significance. Some entries provide international or domestic context for technological development and national policymaking. Moreover, some entries may refer to developments with positive consequences for nonproliferation 2007-2000: NPO MASHINOSTROYENIYA 28 August 2007 NPO MASHINOSTROYENIYA TO FORM CORPORATION NPO Mashinostroyeniya is set to form a vertically-integrated corporation, combining producers and designers of various supply and support elements. The new holding will absorb OAO Strela Production Association (PO Strela), OAO Permsky Zavod Mashinostroitel, OAO NPO Elektromekhaniki, OAO NII Elektromekhaniki, OAO Avangard, OAO Uralskiy NII Kompositsionnykh Materialov, and OAO Kontsern Granit-Elektron. While these entities have acted in coordination for some time, formation of the new corporation has yet to be finalized. -
Sea-Launch for Small Satellites: an American/Russian Joint Venture
I I SEA-LAUNCH FOR SMALL SATELLITES I AN AMERICAN/RUSSIAN JOINT VENTURE I by John E. Draim I Sea-Launch Investors, Inc. Fairfax. Virginia, I I Introduction I Abstract In the last half of the 1990's, there will be a This pap~r describes practical means of dramatic increase in the number of small and I. bypassing the two major impediments to the medium satellites being placed in Low Earth Orbit. commercial exploitation of space. These two Major contributors will be the Big- and Little- LEO impediments. or constraints, are the affordability. commercial communications satellite developers now I reliability. and availability of launch vehicles on the one hand. and the affordability. availability, and I flexibility of launch facilities on the other hand. As to the former, US launch vehicles are noted for their vying for the opportunity to develop satellite based technological complexity, their high cost, and their cellular phone services for vast areas not now I susceptibility to Single point failures. As to the covered by terrestrial cellular providers. Also, latter, our land launch facilities are costly, satellites will be orbited for various types of inadequate and congested. Schedule delays on one observation (landsat, oceanography, weather, ozone I launch cause delays for all succeeding launches sensors. etc.) It appears obvious that lower launch from a given launch pad. costs would also encourage an increase in the popularity of university and amateur scientific I The conversion of suitable military rockets satellites. Capitalizing on the obvious (as well as the (and specifically surplus SLBMs) into satellite launch not-so-obvious) advantages of the floating sea vehicles will use already paid-for assets and will launch, we can provide added flexibility with lower I minimize costs for new construction as well as cost than by merely continuing along the more rocket fuels and oxidizers. -
Failures in Spacecraft Systems: an Analysis from The
FAILURES IN SPACECRAFT SYSTEMS: AN ANALYSIS FROM THE PERSPECTIVE OF DECISION MAKING A Thesis Submitted to the Faculty of Purdue University by Vikranth R. Kattakuri In Partial Fulfillment of the Requirements for the Degree of Master of Science in Mechanical Engineering August 2019 Purdue University West Lafayette, Indiana ii THE PURDUE UNIVERSITY GRADUATE SCHOOL STATEMENT OF THESIS APPROVAL Dr. Jitesh H. Panchal, Chair School of Mechanical Engineering Dr. Ilias Bilionis School of Mechanical Engineering Dr. William Crossley School of Aeronautics and Astronautics Approved by: Dr. Jay P. Gore Associate Head of Graduate Studies iii ACKNOWLEDGMENTS I am extremely grateful to my advisor Prof. Jitesh Panchal for his patient guidance throughout the two years of my studies. I am indebted to him for considering me to be a part of his research group and for providing this opportunity to work in the fields of systems engineering and mechanical design for a period of 2 years. Being a research and teaching assistant under him had been a rewarding experience. Without his valuable insights, this work would not only have been possible, but also inconceivable. I would like to thank my co-advisor Prof. Ilias Bilionis for his valuable inputs, timely guidance and extremely engaging research meetings. I thank my committee member, Prof. William Crossley for his interest in my work. I had a great opportunity to attend all three courses taught by my committee members and they are the best among all the courses I had at Purdue. I would like to thank my mentors Dr. Jagannath Raju of Systemantics India Pri- vate Limited and Prof. -
Existing Space Access for Small Satellites
Existing Space Access for small satellites Future technical trends and possibilities Space Economy in the Multipolar World SEMW2010 1st International Conference, Vilnius, Lithuania, October 6-8, 2010 CNES, Launchers Directorate (Evry, France) – M. Pons, C. Talbot 1 Launchers - Existing launchers - Some projects - quick zoom on MLA project 2 Future trends - Market analysis - Future opportunities SEMW2010 1st International Conference, Vilnius, Lithuania, October 6-8, 2010 All rights reserved © CNES (2010) Page 2 European launchers Europe will soon operate from French Guiana a new family of launchers : Ariane 5, in its last version (A5ECA) using a 14t cryogenic upper stage propelled by HM7 Soyuz, in its “1a” version, will be first launched from Guiana in 2011 Vega, the new developed rocket, will be launched from Kourou by end 2011 This family is adapted to European institutional and commercial needs with a complete coverage of the payloads between small to heavy payloads. SEMW2010 1st International Conference, Vilnius, Lithuania, October 6-8, 2010 All rights reserved © CNES (2010) Page 3 European launchers Current European offer : 200 kg 1.5T 5T Escape Performance ranges of European 400 kg 3T 10T GTO launchers and projects in relation to satellite masses. 200 kg 1.5T 5T MEO 10 kg 100 kg 500 kg 2T 5T 20T LEO Nano Micro Mini Small Medium Heavy Very Small Very Heavy Ariane 5 Vega Soyuz/G 9.5t GTO 1.4t SSO 3t GTO 20t ISS 4.5t SSO 5t Mars 1.5t Mars PERSEUS Project Vega+ project A5ME, BBL & NGL projects ? SEMW2010 1st International Conference, -
Iran's Space Program: Timeline and Technology
Report Iran’s Space Program: Timeline and Technology 29 Apr. 2020 Contents I- Iran’s Space and Satellite Program’s Timeline ..................... 1 II- Satellite and SLV Technology in Iran ................................. 3 Conclusion ...........................................................................6 Iran successfully launched its first dual purpose military-non-military Noor satellite into orbit on April 22, 2020. Produced domestically, the satellite was launched by a new Space Launch Vehicle (SLV), the Qased. The launch publicly disclosed military aspects of Iran’s space program that were previously denied. Noor has increased international concerns over Iran’s hidden Inter- Continental Ballistic Missile Program (ICBM). Iran’s latest satellite technological and military advancement is a far cry from its early commitment to United Nations treaties and principles promoting the peaceful use of space. Iran is a founding member of the United Nations Committee on the Peaceful Uses of Outer Space (COPUOS) launched in December 1958. The following sections review the timeline and technology of Iran’s space program, to show that it had a military component that evolved over time. I- Iran’s Space and Satellite Program’s Timeline Set up over a decade ago, Iran’s satellite and inter-continental missile technology was launched by the Islamic Revolutionary Guard Corps (IRGC)-affiliated Self-Sufficiency Jihad Organization (SSJO). The components of the program were laid out as early as 2004, when Iran established a Supreme Space Council chaired by its sitting president, and monitored by the Iranian Ministry of Communication and Informational Technology.1 In the early stages of Iran’s space program, communication satellites were developed jointly at lower cost with foreign space agencies. -
The Future of North Korean Nuclear Delivery Systems
The Future of North Korean Nuclear Delivery Systems JOHN SCHILLING HENRY KAN APRIL 2015 NORTH KOREA’S NUCLEAR FUTURES SERIES US-KOREA INSTITUTE AT SAIS John Schilling is an aerospace engineer with more than twenty years of experience, specializing in rocket and spacecraft propulsion and mission analysis. Dr. Schilling received his Ph.D. in astronautical engineering from the University of Southern California, and spent most of his career as a contractor for the Air Force Research Laboratory’s Propulsion Directorate. He currently works for the Aerospace Corporation as a specialist in satellite and launch vehicle propulsion systems. Henry (Long) Kan is a Research Assistant at the US-Korea Institute at the Johns Hopkins School of Advanced International Studies (SAIS). His work primarily focuses on nuclear security governance, nuclear command and control systems, and Asia-Pacific maritime security. He holds a B.A. in Political Science and Economics from the University of California, Irvine, where he studied East Asian politics and US national security policy. The Future of North Korean Nuclear Delivery Systems JOHN SCHILLING HENRY KAN APRIL 2015 NORTH KOREA’S NUCLEAR FUTURES SERIES US-KOREA INSTITUTE AT SAIS Copyright © 2015 by the US-Korea Institute at SAIS Printed in the United States of America www.uskoreainstitute.org All rights reserved, except that authorization is given herewith to academic institutions and educators to reproduce for academic use as long as appropriate credit is given to the author and to this publication. The views expressed in this publication are of the authors and do not necessarily represent the opinions of the US-Korea Institute at SAIS.