Toronto: D. Van Nostrand Company, 1958. — 600 p. The guided missile and space slight practitioner will find here the first unclassified complete handbook in his field. Preliminary designs and parametric studies important in weapon system analysis can be made from these equations, formulas, graphs and tables.
Translated from Russian. — Washington: National Aeronautics and Space Administration, 1974. — 208 p. Translation of "Razvitiye Otechestvennogo Raketnogo Dvigatelestroyeniya", Moscow, Mashinostroyeniye Press, 1973. This book covers the history of the creation of Soviet liquid-fueled rocket engines. The works of K. E. Tsiolkovskiy and Yu. V. Kondratyuk on the selection of engine...
Translation Division Foreign Technology Division, 1967. — 356 p. Sourse - "Stale Paliwa Rakietowe". — Warszawa: Wydawnictwo Ministerstwa Obrony Narodowe, 1964. — 300 s. This book is intended for scientific workers interested in combustion problems, for students of higher and middle technical schools, and for technicians. It should be useful to a wide circle of rocket modelers....
Doctoral Dissertation from Doctoral Programme in Mathematical Models and Methods in Engineering. — Milano: Politecnico di Milano: 2014. — 140 p. Hybrid rocket engines are nowadays considered the new frontier for space propulsion due to their low cost, operational flexibility and intrinsic safety. Their multiphase and multi-domain characteristics result in major difficulties in...
Перевод с англ. яз. — М.: Иностранная литература, 1963. — 287 с. В работах американских специалистов по ракетной и космической технике, публикуемых в настоящей книге, обсуждаются вопросы траекторных измерений искусственных спутников и космических ракет. Отдельные статьи посвящены вопросам оптимизации систем траекторных измерений, использованию в них допплеровских методов,...
Kirtland: Office of Aerospace Studie, 1996. — 225 p. The performance of chemical upper stage rocket propulsion cannot be improved much in the near future. However, promising alternative solar- and nuclear-powered upper stages could be operational within ten years. This report provides a detailed discussion of these alternative upper stage concepts and their likely applications...
Technical Manual R3896-11. — Rocketdyne, a division of North American Rockwell Corporation, 1969. — 467 p. This manual contains operating requirements and recommended procedures to support these requirements, for the F-1 Rocket Engine. Operation Requirements . Inspections. Electrical Tests. Leak and Function Tests. Storage Preparation. Servicing. Handling. General Requirements...
М.: Воениздат МО СССР, 1965. — 208 с. В книге излагаются особенности и принципы построения систем навигации. Рассматриваются принципы действия и устройства датчиков первичной навигационной информации. Главное внимание уделяется астрономическим, инерциальным и комплексным системам навигации. Рассказывается об особенностях применения навигационных систем на различных этапах...
Fifth edition. — Washington: Office of Air Force History United States Air Force, 1970. — 101 p. Bibliography of references, periodicals, and educational materials related to space flight.
Technical Note. — Washington: NASA, 1962. — 25 p. Extensive use of the high-energy propellant combination, hydrogen and oxygen, in upper-stage rocket propulsion systems is currently being planned. While this combination has a high specific impulse potential it does have the disadvantage of not being spontaneously ignitable and thus requires the development of a reliable...
М.: Союзинтех, 1967. — 4 с. ORM-1 is an experimental liquid rocket engine. The first one developed in the USSR. It was created in the GDL by V. P. Glushko in 1930-1931. Toluene or gasoline was used as fuel, nitrogen tetraoxide or liquid oxygen was used as an oxidizer. When running on gasoline with liquid oxygen, the thrust reached 200 N. It was cooled with water. The combustion...
М.: Союзинтех, 1968. — 4 с. The RD-214 (GRAU Index 8D59) was a liquid rocket engine, burning AK-27I (a mixture of 73% nitric acid and 27% N2O4 + iodine passivant and TM-185 (a kerosene and gasoline mix) in the gas generator cycle. As was the case with many V-2 influenced engines, the single turbine was driven by steam generated by catalytic decomposition of H2O2. It also had...
М.: Союзинтех, 1968. — 4 с. RD-219 is a derivative of RD-217 with a truss and some piping changes. Despite higher expansion ratio the engine is shorter than first stage engines. The result is relatively low performance, with Isp just 3 sec more than that of 1st stage in vacuum. Engine Cycle: Open. Feed Method: single turbo pump feeding two gimbaled chambers. Diameter is per...
М.: Союзинтех, 1967. — 4 p. The RD-107 and its sibling, the RD-108, are a type of rocket engine initially used to launch R-7 Semyorka missiles. RD-107 engines were later used on space launch vehicles based on the R-7.
М.: Союзинтех, 1967. — 4 с. The RD-119 (GRAU Index 8D710) was a liquid rocket engine, burning liquid oxygen and UDMH in the gas-generator cycle. It has a huge expansion ratio on the nozzle and uses a unique propellant combination to achieve an extremely high isp of 352 s for a semi-cryogenic gas-generator engine. It also has a unique steering mechanism. The engine main nozzle...
Ohaio: Foreign Technology Division, 1962. — 715 p. Sourse (Moscow: Izdatel'stvo Akademii Nauk SSSR, Institut Neftekhimicheskogo Sinteza, 1962. — 437 s. "Topliva Dlya Vozdushno-reaktivnykh i Racetnykh Dvigateley"). The widespread development during the past 10 to 20 years of reaction engineering with its liquid and air-reaction engines was preceded by an extensive period (more...
Proceedings of a Symposium held at ESTEC, Noordwijk, The Netherlands, 2-5 October 1979. — 323 p. Project tenagers are also rather conservative and can be driven to adopt new approaches only if old ones are shewn to be inadequate. There is a lack of incentive, when came to the mass production industry, to avoid firstly over designing with consequent, and secondly, failures after...
Washington: NASA, 1967. — 460 p. From the component design to the subsystem design to the engine systems design, engine development, and flight-vehicle application, this how-to text bridges the gap between basic physical and design principles and actual rocket-engine design as it's done in industry. More than 470 illustrations and tables help to make this book a must-read for...
The Boeing Conpany, 1968. — 185 p. This document contains information on rocket engines using propellants stored as liquids or gases. Volume 1 contains information on engines used for reaction control systems and low velocity increment propulsion systems. Cold (ambient) gas, heated gas, monopropellant and bipropellant engines are considered. Estimates are made of performance,...
Patterson Air Force Base: Foreign Technology Division, 1972. — 138 p. This textbook rives a general survey, classification, and brief description of rocket engines and their working substances. It's presents briefly the history of the development of rocket engines. It examines the theory of thermal rocket engines and presents the principles for the construction and design of...
Translation of "Kosmicheskiye zhidkostno-raketnyye dvigateli", Novoe v zhizni, nauke, tekhnike; Seriya "Kosmonavtika, astronomiya," No. 9, 1976. — Washington: National Aeronautics and Space Administration, 1976. — 64 p. Liquid rocket engines (ZhRD), which operate on liquid fuel, along with solid fuel rocket engines (RDTT) are the main types of space engines. They are used...
Arlington: Office of Naval Research, 1971. — 870 p. In the structural integrity analysis of solid rocket propellant motors, intrinsic material and geometric complexities, such as interrelated thme, temperature and shape dependent grain response, have dictated many simplifying assw-aptions which are becoming increasingly incompatible with rising performance requirements. While...
SUSTAIN Conference briefing XCOR Aerospace, 2009. — 15 p. Company Status (XCOR in 60 sec) Lynx Flight Profile Operating Advantages Lynx and Lynx II Other missions Other missions relevant to DoD Update - Progress in Last 30 Days SUSTAIN & Similar Missions How to get there? Past Paradigms Notional architectures for full SUSTAIN Ingress Extraction The point
М.: Изд-во иностранной литературы, 1958. — 304 с.: ил. В книге английского специалиста по ракетной технике Дж. Хэмфриса рассматриваются вопросы устройства ракетных двигателей на твердом и жидком топливе и различные области их применения, главным образом для управляемых снарядов. Даются также основные сведения об управляемых снарядах ближнего действия и дальнобойных...
М.: Воениздат, 1975. — 168 с., ил. В книге излагается принцип работы инерциальной системы, описываются методы подготовки ее к работе и сам процесс инерциального управления ракетами, стартующими со стационарных и подвижных пусковых устройств. Показаны пути повышения точности инерциального наведения, описываются типовые инерциальные системы, используемые в ракетной технике за...
М.: Машиностроение, 1970. — 366 с. Книга написана известными американскими учеными и специалистами в области космической навигации, конструирования систем наведения и стабилизации. В ней изложены принципы и методы проектирования систем управления для космических аппаратов. Даны решения задач с иллюстрациями на конкретном примере американского космического корабля «Аполлон»....
Washington: National Aeronautics and Space Administration, 1970. — 1047 p. Английский перевод книги Н. Ф. Краснова "Аэродинамика ракет". The Concepts of Forces, Moments, and Aerodynamic Coefficients Shapes of the Vehicles and Their Elements Fundamental Relationships in the Theory of Gas Flows General Methods of Solution of Aerodynamic Problems Calculation of the Aerodynamic...
Koln: NATO, 1976. — 154 p. The specialists meeting is devoted to technological problems associated with propulsion systems of advanced small rocket motors for anti-tank , anti-aircraft , and light artillery rockets. After specification of the requirements for the three types of weapon systems , problems of systems development will be discussed including the optimization and...
Denisov V.P., Yermilov A.A., Zhelyabin B.I., Kirsanov A.V., Leonidov I.L., Polyakov V.A., Timonin A.A., Tumanov A.M., Narimanov G.S. — Second edition. — Moscow: Mashinostroenie, 1971. — 128 p. The Soviet manned space program is discussed. The main stages of development of Soviet cosmonautics are considered, as well as the program for the manned spacecraft Vostok, Voskhod and...
AGARD Conference Proceedings N279. — NATO: 1979. — 536 p. Survey Papers; Ignition, Extinction and Internal Ballistics; Burn Rate Modelling and Combustion of Metal; New Propellants; Combustion Instability; Heat Transfer and Materials; Testing and Instrumentation.
AGARD Conference Proceedings N279. — NATO: 1979. — 536 p. Survey Papers; Ignition, Extinction and Internal Ballistics; Burn Rate Modelling and Combustion of Metal; New Propellants; Combustion Instability; Heat Transfer and Materials; Testing and Instrumentation.
Clarke V.C., Bollman W.E., Roth R.Y., Scholey W.J. — Washington: NASA, 1963. — 398 p. Design parameters for ballistic interplanetary trajectories - Mars and Venus one-way transfers. The general characteristics of ballistic interplanetary trajectories are discussed, and detailed equations are developed for the analytical model. Extensive data are presented in graphical form for...
Hampton: Space Administration Office of Management Scientific and Technical Information Division, 1990. — 73 p. With the use of an operational space station as an initial staging node in low-Earth orbit (LEO), recent studies (refs. 1 and 2) have shown that manned exploration of the solar system will be technically feasible early in the 21st century. Because of its proximity,...
Second edition. — Washington: Office of Air Force History United States Air Force, 1986. — 341 p. Seventy years have passed since August 1908 when the Wright brothers delivered the world's first military aircraft to the United States government. This momentous event stimulated immense public interest and prompted an outpouring of newspaper and magazine articles. Interest in...
Alabama: Space Flight Center, 1984. — 322 p. A preliminary spacecraft servicing demonstration plan is prepared which leads to a fully verified operational on-orbit servicing system based on the module exchange, refueling, and resupply technologies. The resulting system can be applied at the space station, in low Earth orbit with an orbital maneuvering vehicle (OMV), or be carried...
Translated and Edited by H. Needler. — Moskva: Izdatel’stvo Akademii Nauk SSSR, 1963. — 236 p. A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants (fuel/oxidizer). The earliest rockets were solid-fuel rockets powered by gunpowder; they were used in warfare by the Chinese, Indians, Mongols and Persians, as early as the 13th...
A Dissertation Submitted to the Faculty of Purdue University In Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy. — West Lafayette: Purdue University, 2010. — 235 p. Currently, NASA is preparing to launch the Gravity Recovery and Interior Laboratory (GRAIL) on September 6, 2011. Besides adding to the scientific understanding of the Moon’s internal...
Washington: National Aeronautics and Space Administration, 2006. — 659 p. An engrossing read, Critical Issues in the History of Spaceflight is a volume consisting of scholarship on the current state of the discipline of space history presented in a joint NASA and NASM conference in 2005. The essays presented in the book question such issues as the motivations of spaceflight, and...
Master of Science Thesis. — For the degree of Master of Science in Aerospace Engineering at the Delft University of Technology, 2015. — 118 p. Unperturbed observation of deep space radio waves is impossible to achieve from Earth but could be managed if the instruments were positioned in a place shielded from Earth, such as the far side of the Moon or the Shackleton crater,...
Leadership Development and Membership Services Directorate, Alabama, 2003. — 86 p. This pamphlet was designed to be a transition from Module 4, ROCKETS, of Aerospace Dimensions, into the hobby and science of model rocketry. The author starts out with simple alternative-power models and progressively challenges the cadet with more advanced models. This publication is about the...
Engineering and Development Company, USA, 1979. — 49 p. The information contained in this text is intended for the serious experimenter and should be used only by those with a thorough background knowledge in model rocketry. Commercially manufactured model rocket engines and model rocket kits are readily available and should be used by beginners. Model rocket engines built by the...
Институт сильноточной электроники СО РАН. — Томск, 2014. — 137 с. Отчет о прикладных научных исследованиях. Объектами исследования является экспериментально-аппаратный комплекс, реализующий методику комплексного тестирования модулей бортовой аппаратуры и кабельной сети космических аппаратов на устойчивость к дугообразованию, и экспериментальный образец программного комплекса,...
Бармин И.В., Климов В.Н., Рахманов Ж.Р., Сборец В.П., Игнашин А.М. B64G5/00 Наземное оборудование для космических кораблей, например стартовые установки, оборудование для заправки топливом. Подача заявки: 2004-08-05. — 12 с. Изобретение относится к наземному оборудованию для космических кораблей. Предлагаемый стартовый комплекс содержит центр управления запуском,...
СПб.: Санкт-Петербургский национальный исследовательский университет информационных технологий, механики и оптики, 2012. — 27 с. Основные сведения о космодромах. Основные сведения о позиционном районе ракетно-космических комплексов. Общие сведения о технологическом оборудовании ракетно-космических комплексов. Понятие обобщенного технологического процесса. Содержание и...
Диссертация на соискание ученой степени кандидата экономических наук. Специальность 08.00.05 – Экономика и управление народным хозяйством (экономика, организация и управление предприятиями, отраслями, комплексами – транспорт). — М.: Государственный университет управления, 2014. — 175 с. Научный руководитель: дэн Савченко-Бельский В.Ю. Введение Характеристика процессов...
Мальцев Ю.А. ВКР. — Томск, ТГУ, 2015. — 89 с. Объектом исследования является высокодетальный космический аппарат оптического наблюдения. Цель работы – разработка технических предложений на высокодетальный космический аппарат оптического наблюдения. С этой целью в результате выполнения работ были сформулированы основные требования к разрабатываемому высокодетальному космическому...
Пособие по выполнению контрольных работ. — М.: МГТУ ГА, 2014. — 20 с. Данное пособие издается в соответствии с рабочей программой учебной дисциплины «История авиации и космонавтики» по Учебному плану для студентов I-II курсов всех направлений и специальностей заочной формы обучения. Цель и задачи контрольной работы: на основе самостоятельного изучения темы курса «История...
Автореферат диссертации на соискание ученой степени кандидата технических наук. Специальность 05.09.03 – электротехнические комплексы и системы. — Красноярск, СФУ, 2009. — 20 с. Современные требования к выходному импедансу систем электропитания (СЭП) космических аппаратов (КА) значительно жестче требований, предъявляемых к СЭП 70-х, 80-х годов прошлого века. Необходимость в...