Russian Rocket Engines Used by the United States
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RD-180—Or Bust?
RD-180—or By Autumn A. Arnett, Associate Editor As it stands, the US could sustain its Bust? manifest for two years with the current supply of RD-180 engines. But a new he United States’ sustained access he doesn’t really know what that R&D engine could take seven or more years to space is in question. Heavily amounts to, but said he is hopeful the to be operational, making LaPlante’s Treliant on the Russian-made En- partnership will mean a new engine on “$64 million question” a “hydra-headed ergomash RD-180 engine to power its the market soon. monster,” in the words of former AFSPC launches, US military space personnel “Three years of development is better Commander Gen. William L. Shelton. are looking for a replacement because than starting at ground zero,” Hyten said. “I don’t think we build the world’s best of the tense and uncertain status of “If we start at ground zero to build a rocket engine,” Shelton said last July. “I American and Russian relations. new engine in the hydrocarbon technology would love for us as a nation to regain the Funds are already being appropriated area we’re fi ve years away from produc- lead in liquid rocket propulsion.” for research and development of a new tion, roughly, maybe four, maybe six. Both LaPlante and Hyten are propo- engine, but Gen. John E. Hyten, com- The one thing you would have to do is nents of the United States continuing to mander of Air Force Space Command, spend the next year or two driving down fund research and development of a new considers the issue to be urgent. -
ULA Atlas V Launch to Feature Full Complement of Aerojet Rocketdyne Solid Rocket Boosters
April 13, 2018 ULA Atlas V Launch to Feature Full Complement of Aerojet Rocketdyne Solid Rocket Boosters SACRAMENTO, Calif., April 13, 2018 (GLOBE NEWSWIRE) -- The upcoming launch of the U.S. Air Force Space Command (AFSPC)-11 satellite aboard a United Launch Alliance Atlas V rocket from Cape Canaveral Air Force Station, Florida, will benefit from just over 1.74 million pounds of added thrust from five AJ-60A solid rocket boosters supplied by Aerojet Rocketdyne. The mission marks the eighth flight of the Atlas V 551 configuration, the most powerful Atlas V variant that has flown to date. The Atlas V 551 configuration features a 5-meter payload fairing, five AJ-60As and a Centaur upper stage powered by a single Aerojet Rocket RL10C-1 engine. This configuration of the U.S. government workhorse launch vehicle is capable of delivering 8,900 kilograms of payload to geostationary transfer orbit (GTO), and also has been used to send scientific probes to explore Jupiter and Pluto. The Centaur upper stage also uses smaller Aerojet Rocketdyne thrusters for pitch, yaw and roll control, while both stages of the Atlas V employ pressurization vessels built by Aerojet Rocketdyne's ARDÉ subsidiary. "The Atlas V is able to perform a wide variety of missions for both government and commercial customers, and the AJ-60A is a major factor in that versatility," said Aerojet Rocketdyne CEO and President Eileen Drake. "Aerojet Rocketdyne developed the AJ-60A specifically for the Atlas V, delivering the first booster just 42 months after the contract award, which underscores our team's ability to design and deliver large solid rocket motors in support of our nation's strategic goals and efforts to explore our solar system." The flight of the 100th AJ-60A, the largest monolithically wound solid rocket booster ever flown, took place recently as part of a complement of four that helped an Atlas V 541 place the nation's newest weather satellite into GTO. -
6. Chemical-Nuclear Propulsion MAE 342 2016
2/12/20 Chemical/Nuclear Propulsion Space System Design, MAE 342, Princeton University Robert Stengel • Thermal rockets • Performance parameters • Propellants and propellant storage Copyright 2016 by Robert Stengel. All rights reserved. For educational use only. http://www.princeton.edu/~stengel/MAE342.html 1 1 Chemical (Thermal) Rockets • Liquid/Gas Propellant –Monopropellant • Cold gas • Catalytic decomposition –Bipropellant • Separate oxidizer and fuel • Hypergolic (spontaneous) • Solid Propellant ignition –Mixed oxidizer and fuel • External ignition –External ignition • Storage –Burn to completion – Ambient temperature and pressure • Hybrid Propellant – Cryogenic –Liquid oxidizer, solid fuel – Pressurized tank –Throttlable –Throttlable –Start/stop cycling –Start/stop cycling 2 2 1 2/12/20 Cold Gas Thruster (used with inert gas) Moog Divert/Attitude Thruster and Valve 3 3 Monopropellant Hydrazine Thruster Aerojet Rocketdyne • Catalytic decomposition produces thrust • Reliable • Low performance • Toxic 4 4 2 2/12/20 Bi-Propellant Rocket Motor Thrust / Motor Weight ~ 70:1 5 5 Hypergolic, Storable Liquid- Propellant Thruster Titan 2 • Spontaneous combustion • Reliable • Corrosive, toxic 6 6 3 2/12/20 Pressure-Fed and Turbopump Engine Cycles Pressure-Fed Gas-Generator Rocket Rocket Cycle Cycle, with Nozzle Cooling 7 7 Staged Combustion Engine Cycles Staged Combustion Full-Flow Staged Rocket Cycle Combustion Rocket Cycle 8 8 4 2/12/20 German V-2 Rocket Motor, Fuel Injectors, and Turbopump 9 9 Combustion Chamber Injectors 10 10 5 2/12/20 -
Jpc-Final-Program.Pdf
49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit (JPC) Advancing Propulsion Capabilities in a New Fiscal Reality 14–17 July 2013 San Jose Convention Center 11th International Energy Conversion San Jose, California Engineering Conference (IECEC) FINAL PROGRAM www.aiaa.org/jpc2013 www.iecec.org #aiaaPropEnergy www.aiaa.org/jpc2013 • www.iecec.org 1 #aiaaPropEnergy GET YOUR CONFERENCE INFO ON THE GO! Download the FREE Conference Mobile App FEATURES • Browse Program – View the program at your fingertips • My Itinerary – Create your own conference schedule • Conference Info – Including special events • Take Notes – Take notes during sessions • Venue Map – San Jose Convention Center • City Map – See the surrounding area • Connect to Twitter – Tweet about what you’re doing and who you’re meeting with #aiaaPropEnergy HOW TO DOWNLOAD Any version can be run without an active Internet connection! You can also sync an Compatible with itinerary you created online with the app by entering your unique itinerary name. iPhone/iPad, MyItinerary Mobile App MyItinerary Web App Android, and • For optimal use, we recommend • For optimal use, we recommend: rd BlackBerry! iPhone 3GS, iPod Touch (3 s iPhone 3GS, iPod Touch (3rd generation), iPad iOS 4.0, or later generation), iPad iOS 4.0, • Download the MyItinerary app by or later searching for “ScholarOne” in the s Most mobile devices using Android App Store directly from your mobile 2.2 or later with the default browser device. Or, access the link below or scan the QR code to access the iTunes s BlackBerry Torch or later device Sponsored by: page for the app. -
Materials for Liquid Propulsion Systems
https://ntrs.nasa.gov/search.jsp?R=20160008869 2019-08-29T17:47:59+00:00Z CHAPTER 12 Materials for Liquid Propulsion Systems John A. Halchak Consultant, Los Angeles, California James L. Cannon NASA Marshall Space Flight Center, Huntsville, Alabama Corey Brown Aerojet-Rocketdyne, West Palm Beach, Florida 12.1 Introduction Earth to orbit launch vehicles are propelled by rocket engines and motors, both liquid and solid. This chapter will discuss liquid engines. The heart of a launch vehicle is its engine. The remainder of the vehicle (with the notable exceptions of the payload and guidance system) is an aero structure to support the propellant tanks which provide the fuel and oxidizer to feed the engine or engines. The basic principle behind a rocket engine is straightforward. The engine is a means to convert potential thermochemical energy of one or more propellants into exhaust jet kinetic energy. Fuel and oxidizer are burned in a combustion chamber where they create hot gases under high pressure. These hot gases are allowed to expand through a nozzle. The molecules of hot gas are first constricted by the throat of the nozzle (de-Laval nozzle) which forces them to accelerate; then as the nozzle flares outwards, they expand and further accelerate. It is the mass of the combustion gases times their velocity, reacting against the walls of the combustion chamber and nozzle, which produce thrust according to Newton’s third law: for every action there is an equal and opposite reaction. [1] Solid rocket motors are cheaper to manufacture and offer good values for their cost. -
Los Motores Aeroespaciales, A-Z
Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 < aeroteca.com > Depósito Legal B 9066-2016 Título: Los Motores Aeroespaciales A-Z. © Parte/Vers: 1/12 Página: 1 Autor: Ricardo Miguel Vidal Edición 2018-V12 = Rev. 01 Los Motores Aeroespaciales, A-Z (The Aerospace En- gines, A-Z) Versión 12 2018 por Ricardo Miguel Vidal * * * -MOTOR: Máquina que transforma en movimiento la energía que recibe. (sea química, eléctrica, vapor...) Sponsored by L’Aeroteca - BARCELONA ISBN 978-84-608-7523-9 Este facsímil es < aeroteca.com > Depósito Legal B 9066-2016 ORIGINAL si la Título: Los Motores Aeroespaciales A-Z. © página anterior tiene Parte/Vers: 1/12 Página: 2 el sello con tinta Autor: Ricardo Miguel Vidal VERDE Edición: 2018-V12 = Rev. 01 Presentación de la edición 2018-V12 (Incluye todas las anteriores versiones y sus Apéndices) La edición 2003 era una publicación en partes que se archiva en Binders por el propio lector (2,3,4 anillas, etc), anchos o estrechos y del color que desease durante el acopio parcial de la edición. Se entregaba por grupos de hojas impresas a una cara (edición 2003), a incluir en los Binders (archivadores). Cada hoja era sustituíble en el futuro si aparecía una nueva misma hoja ampliada o corregida. Este sistema de anillas admitia nuevas páginas con información adicional. Una hoja con adhesivos para portada y lomo identifi caba cada volumen provisional. Las tapas defi nitivas fueron metálicas, y se entregaraban con el 4 º volumen. O con la publicación completa desde el año 2005 en adelante. -Las Publicaciones -parcial y completa- están protegidas legalmente y mediante un sello de tinta especial color VERDE se identifi can los originales. -
NASA News National Aeronautics and Space Administration Washington
NASA News National Aeronautics and Space Administration Washington. D C 20546 AC 202 755-8370 For Release IMMEDIATE Press Kit Project Intelsat V-D RELEASE NO: 82-30 Contents GENERAL RELEASE 1 ATLAS CENTAUR, LAUNCH VEHICLE STATISTICS 3 LAUNCH OPERATIONS 4 LAUNCH SEQUENCE FOR INTELSAT V-D 5 THE NASA INTELSAT TEAM 6 CONTRACTORS 7 /lNASA-News-Belease-82^TOl INTELSAT N82-22295 "\ (SATELLITE SCHEDULED FOR LAUNCH (National (Aeronautics and Space Administration) 8 p I CSCL 22A Unclas I 00/15 18771 February 26, 1982 NASA News National Aeronautics and Space Administration Washington. D C 20546 AC 202 755-8370 For Release Dick McCormack Headquarters, Washington, D.C. IMMEDIATE (Phone: 202/755-8104) RELEASE NO: 82-30 INTELSAT SATELLITE SCHEDULED FOR LAUNCH Intelsat V-D, the fourth of a new series of nine inter- national telecommunications satellites owned and operated by the 105-nation International Telecommunications Satellite Organiza- tion (Intelsat), is scheduled to be launched by the NASA Kennedy Space Center on board an Atlas Centaur launch vehicle no earlier than March 4, 1982, from Cape Canaveral, Fla. The three Intelsat Vs were successfully launched by NASA in December 1980, May 1981 and December 1981. Intelsat V-D weighs 1,928 kilograms (4,251 pounds) at launch and has almost double the communications capability of early satellites in the Intelsat series — 12,000 voice circuits and two color television channels. It will be positioned in geosyn- chronous orbit over the Indian Ocean as the prime Intelsat satel- lite to provide communications services between Europe, the Middle East and the Far East. -
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. -
Commercialization of Russian Technology in Cooperation with American Companies
Stanford University CISAC Center for International Security and Cooperation The Center for International Security and Cooperation, part of Stanford University’s Institute for International Studies, is a multidisciplinary community dedicated to research and train- ing in the field of international security. The Center brings together scholars, policymakers, scientists, area specialists, members of the business community, and other experts to examine a wide range of international security issues. Center for International Security and Cooperation Stanford University Encina Hall Stanford, California 94305-6165 (415) 723-9625 http://www.stanford.edu/group/CISAC/ Commercialization of Russian Technology in Cooperation with American Companies David Bernstein June 1999 David Bernstein, an engineering research associate at Stanford University’s Center for Inter- national Security and Cooperation, participates in the Center’s Project on Industrial Restruc- turing and the Political Economy in Russia. The opinions expressed here are those of the author and do not represent positions of the Center, its supporters, or Stanford University. © 1999 by the Board of Trustees of the Leland Stanford Junior University ISBN 0-935371-53-2 i ii Contents I. Introduction 1 II. Background 5 III. Case Studies Introduction to Case Studies 17 Air Products & Chemicals, Incorporated 19 Boeing 21 Corning, Incorporated 27 Energia, Ltd. 29 NPO Energomash 33 FMC 37 General Electric 41 The State Scientific Research Institute of Aviation Systems (GosNIIAS) 43 Karpov Institute -
Do Not Circulate
LA-7328-PR Progress Report a . Laser Fusion Program July 1—December 31, 1977 ,- .. .. .. ..-— — DO NOT CIRCULATE PERMANENT RETENTION ! REQUIREDBY CONTRACT v LOS ALAMOS SCIENTIFIC LABORATORY Lail!lik — post Office Box 1663 Los Alamos, New Mexico 87545 An AffumativeAction/EqualOpportunityEmployex . The four most recent reports in this series,un- classified, are LA-65 10-PR, LAY6 16-PR, LA4834-PR, and LA-6982-PR. This work was supported by the US Department of Energy, Office of Laser Fusion. TM. report was prep.rcd as m .CLWUII1O( work sponsored by the United SUICS Go”enlme”l. Neither the Un,ted Stiles I nor the United Slates Department cd Enersy. nor any of their employees. nor any 0( their CO.114C10rS. subcontrar tom. or their ●w.loyecs. makes any warranty. .xD,,!s O, irnPlled. ., P .isume. any Iesal Ii. biiity or responsibkbw for the accuracy. cmnpletcncm. y usefulness of any information. app.; .t.s. product. or Pro..= dl=losed. or rrpreacnm that its w would “.1 i“fri”le privately owned rlthls. UNITED STATES DEPARTMENT OF CNCRGV CONTRACT W-7408 -CNO. S6 LA-7328-PR Progress Report UC-21 IssI,W: December 1978 . Laser Fusion Program at LASL July 1—December 31, 1977 Compiled by Frederick Skoberne 4 .! L-. — .— - . ABSTRACT . ...”” 1 SUMMARY . ...0000oo 2 Introduction . 2 CO, Laser Program . 2 Antares . 2 CO, Laser Technology . 3 Laser Fusion Theory, Experiments, and Target Design . 3 Laser Fusion Target Fabrication . 4 1, CO, LASER PROGRAM . 6 Single-Beam System . 6 llvo-Beam System . 6 Eight-Beam System . 8 II. ANTARES-HIGH-ENERGY GAS IJM3ERFAClLITY . -
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 . -
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.