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Статті в журналах з теми "Rocket engines – Design and construction"
Zosimovych, Nickolay. "Sounding Rocket Preliminary Design." European Journal of Engineering and Technology Research 6, no. 2 (February 23, 2021): 136–41. http://dx.doi.org/10.24018/ejers.2021.6.2.2368.
Повний текст джерелаZosimovych, Nickolay. "Sounding Rocket Preliminary Design." European Journal of Engineering and Technology Research 6, no. 2 (February 23, 2021): 136–41. http://dx.doi.org/10.24018/ejeng.2021.6.2.2368.
Повний текст джерелаПалюх, Алексей Владимирович, Сергей Александрович Мотылев та Леонид Прокофьевич Малый. "КОНСТРУКТОРСКОЕ И ТЕХНОЛОГИЧЕСКОЕ ОБЕСПЕЧЕНИЕ ИЗГОТОВЛЕНИЯ КОРПУСА РАКЕТНОГО ДВИГАТЕЛЯ НА ТВЕРДОМ ТОПЛИВЕ ТИПА “КОКОН”". Aerospace technic and technology, № 8 (31 серпня 2019): 22–27. http://dx.doi.org/10.32620/aktt.2019.8.04.
Повний текст джерелаЗолотько, Олександр Євгенович, Олена Василівна Золотько, Олександра Валеріївна Сосновська, Олександр Сергійович Аксьонов та Ірина Сергіївна Савченко. "ОСОБЛИВОСТІ КОНСТРУКТИВНИХ СХЕМ ДВИГУНІВ З ІМПУЛЬСНИМИ ДЕТОНАЦІЙНИМИ КАМЕРАМИ". Aerospace technic and technology, № 2 (27 квітня 2020): 4–10. http://dx.doi.org/10.32620/aktt.2020.2.01.
Повний текст джерелаRicci, Daniele, Francesco Battista, and Manrico Fragiacomo. "Transcritical Behavior of Methane in the Cooling Jacket of a Liquid-Oxygen/Liquid-Methane Rocket-Engine Demonstrator." Energies 15, no. 12 (June 7, 2022): 4190. http://dx.doi.org/10.3390/en15124190.
Повний текст джерелаTakao, Y., T. Shibui, and S. Saito. "A Design and Construction of Civil Work for Rocket Engine Firing Test Facilities." Concrete Journal 27, no. 6 (1989): 38–46. http://dx.doi.org/10.3151/coj1975.27.6_38.
Повний текст джерелаPîslaru-Dănescu, Lucian, Alexandru-Mihail Morega, Rareş-Andrei Chihaia, Ionel Popescu, Mihaela Morega, Lică Flore, Marius Popa, and Eros-Alexandru Pătroi. "New Type of Linear Magnetostrictive Motor Designed for Outer Space Applications, from Concept to End-Product." Actuators 10, no. 10 (October 14, 2021): 266. http://dx.doi.org/10.3390/act10100266.
Повний текст джерелаBudur, О., S. Nikul, M. Petrushenko, V. Holovan, O. Serheyev, and S. Tarasenko. "DEVELOPMENT OF RECOMMENDATIONS FOR CALCULATING THE MECHANISM OF SEPARATION OF PERSPECTIVE SOLID PROPELLANT ROCKETS WITH A NEGATIVE IN-FLIGHT WARHEAD AND MECHANISM OF SEPARATION." Collection of scientific works of Odesa Military Academy 1, no. 12 (December 27, 2019): 81–88. http://dx.doi.org/10.37129/2313-7509.2019.12.1.81-88.
Повний текст джерелаSomov, V. V. "DETERMINATION OF THE TYPE OF A SINGLE-USE GRENADE LAUNCHER BASED ON ITS COMPOSITE PARTS AND FRAGMENTS OF REACTIVE GRENADE FOUND AT THE PLACE OF ACCIDENT." Theory and Practice of Forensic Science and Criminalistics 17 (November 29, 2017): 245–52. http://dx.doi.org/10.32353/khrife.2017.31.
Повний текст джерелаWisniewski, Adam, Maciej Malicki, and Wojciech Manaj. "Visual and microscopic examination of the rocket engine combustion chamber." Aircraft Engineering and Aerospace Technology 92, no. 3 (February 18, 2019): 368–75. http://dx.doi.org/10.1108/aeat-06-2018-0166.
Повний текст джерелаДисертації з теми "Rocket engines – Design and construction"
Baig, Saood Saeed. "A simple moving boundary technique and its application to supersonic inlet starting /." Thesis, McGill University, 2008. http://digitool.Library.McGill.CA:80/R/?func=dbin-jump-full&object_id=112555.
Повний текст джерелаThe developed technique is rather general and can be used with virtually any finite-volume or finite-difference scheme, since the modifications of the schemes themselves are not required. In the present study the proposed technique has been incorporated into a one-dimensional non-adaptive Euler code and a two-dimensional locally adaptive unstructured Euler code.
It is shown that the new approach is conservative with the order of approximation near the moving boundaries. To reduce the conservation error, it is beneficial to use the method in conjunction with local grid adaptation.
The technique is verified for a number of one and two dimensional test cases with analytical solutions. It is applied to the problem of supersonic inlet starting via variable geometry approach. At first, a classical starting technique of changing exit area by a moving wedge is numerically simulated. Then, the feasibility of some novel ideas such as a collapsing frontal body and "tractor-rocket" are explored.
Miller, Robert E. Hartfield Roy J. "Design and testing of a gas distribution method for pulsed inductive thruster." Auburn, Ala, 2008. http://hdl.handle.net/10415/1405.
Повний текст джерелаDoan, Andrew W. "3-D flow and performance of a rocket pump inducer at design and off-design flow rates." Thesis, This resource online, 1994. http://scholar.lib.vt.edu/theses/available/etd-11242009-020251/.
Повний текст джерелаRuss, David Phillip. "Analysis of a heavy lift launch vehicle design using small liquid rocket engines." Thesis, Massachusetts Institute of Technology, 1988. http://hdl.handle.net/1721.1/35340.
Повний текст джерелаDenton, Brandon Lee. "Design and analysis of rocket nozzle contours for launching pico-satellites /." Online version of thesis, 2008. http://hdl.handle.net/1850/6003.
Повний текст джерелаDausen, David F. "Design of a premixed gaseous rocket engine injector for ethylene and oxygen." Thesis, Monterey, Calif. : Naval Postgraduate School, 2006. http://bosun.nps.edu/uhtbin/hyperion.exe/06Dec%5FDausen.pdf.
Повний текст джерелаThesis Advisor(s): Christopher M. Brophy. "December 2006." Includes bibliographical references (p. 97). Also available in print.
Cunha, Marco Antonio Hidalgo. "A computational tool for the design and optimization of supersonic turbines with application on turbopump rocket engines." Instituto Tecnológico de Aeronáutica, 2012. http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=3218.
Повний текст джерелаEbaid, Munzer Shehadeh Yousef. "Design and construction of a small gas turbine to drive a permanent magnet high speed generator." Thesis, University of Hertfordshire, 2002. http://hdl.handle.net/2299/14046.
Повний текст джерелаTam, Kuok San. "Design and analysis of an electro-hydro-mechanical variable valve actuator for four-stroke automobile engines." Thesis, University of Macau, 2011. http://umaclib3.umac.mo/record=b2493685.
Повний текст джерелаJosselyn, Scott B. "Optimization of low thrust trajectories with terminal aerocapture." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion-image/03Jun%5FJosselyn.pdf.
Повний текст джерелаThesis advisor(s): I. Michael Ross, Steve Matousek. Includes bibliographical references (p. 149-150). Also available online.
Книги з теми "Rocket engines – Design and construction"
Hindley, Keith B. Handbook of Russian rocket engines. York: Technology Detail, 1997.
Знайти повний текст джерелаBolonkin, Alexander. The development of Soviet rocket engines (for strategic missiles). Falls Church, VA: Delphic Associates, 1991.
Знайти повний текст джерелаGrishin, S. D. Proektirovanie kosmicheskikh apparatov s dvigateli͡a︡mi maloĭ ti͡a︡gi. Moskva: Mashinostroenie, 1990.
Знайти повний текст джерелаBelov, B. L. Razvitie teorii raketnykh dvigateleĭ: Do 40-kh godov XX stoletii︠a︡. Moskva: Institut istorii estestvoznanii︠a︡ i tekhniki RAN (IIET), 2006.
Знайти повний текст джерелаYe ti huo jian fa dong ji tui li shi she ji: Design for Thrust Chamber of Liquid Propellant Rocket Engines. Beijing Shi: Guo fang gong ye chu ban she, 2014.
Знайти повний текст джерелаI︠A︡godnikov, D. A. Raketno-kosmicheskie dvigatelʹnye ustanovki: Materialy Vserossiĭskoĭ nauchno-tekhnicheskoĭ konferent︠s︡ii, Moskva, okti︠a︡brʹ 2013. Moskva: IIU MGOU, 2013.
Знайти повний текст джерелаV, Glushko A., ed. Valentin Glushko: Konstruktor raketnykh dvigateleĭ i kosmicheskikh sistem. Sankt-Peterburg: Politekhnika, 2008.
Знайти повний текст джерелаOstapenko, I︠U︡ A. Raketoĭ sverknuvshai︠a︡ zhiznʹ: Stranit︠s︡y zhizni vydai︠u︡shchegosi︠a︡ konstruktora aviat︠s︡ionnoĭ i raketnoĭ tekhniki Aleksandra I︠A︡kovlevicha Berezni︠a︡ka. Dubna: Feniks+, 2012.
Знайти повний текст джерелаYe ti huo jian fa dong ji xian dai gong cheng she ji. Beijing shi: Zhongguo yu hang chu ban she, 2004.
Знайти повний текст джерелаYe ti huo jian fa dong ji xian dai gong cheng she ji. Beijing shi: Zhongguo yu hang chu ban she, 2004.
Знайти повний текст джерелаЧастини книг з теми "Rocket engines – Design and construction"
Straub, D. "Design Criteria for Rocket Engines." In Thermofluiddynamics of Optimized Rocket Propulsions, 51–62. Basel: Birkhäuser Basel, 1989. http://dx.doi.org/10.1007/978-3-0348-9150-9_5.
Повний текст джерелаPastrone, Dario, and Lorenzo Casalino. "Optimal Robust Design of Hybrid Rocket Engines." In Springer Optimization and Its Applications, 269–85. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-41508-6_10.
Повний текст джерелаMorgenweck, Daniel, Jutta Pieringer, and Thomas Sattelmayer. "Numerical Determination of Nozzle Admittances in Rocket Engines." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 579–86. Berlin, Heidelberg: Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-14243-7_71.
Повний текст джерелаTraxinger, Christoph, Julian Zips, Christian Stemmer, and Michael Pfitzner. "Numerical Investigation of Injection, Mixing and Combustion in Rocket Engines Under High-Pressure Conditions." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 209–21. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_13.
Повний текст джерелаFiedler, Torben, Joachim Rösler, Martin Bäker, Felix Hötte, Christoph von Sethe, Dennis Daub, Matthias Haupt, Oskar J. Haidn, Burkard Esser, and Ali Gülhan. "Mechanical Integrity of Thermal Barrier Coatings: Coating Development and Micromechanics." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 295–307. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_19.
Повний текст джерелаManikandan, Kabaleeswaran, Boyapati Krishna Vamsi, Pola Anusha, and Chaturya Reddy. "Analysis of Internal Hydrodynamic Behavior of Pressure Swirl Atomizer for Liquid Rocket Engines." In Advances in Design and Thermal Systems, 261–70. Singapore: Springer Singapore, 2021. http://dx.doi.org/10.1007/978-981-33-6428-8_20.
Повний текст джерелаArmbruster, Wolfgang, Justin S. Hardi, and Michael Oschwald. "Experimental Investigation of Injection-Coupled High-Frequency Combustion Instabilities." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 249–62. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_16.
Повний текст джерелаPerakis, Nikolaos, and Oskar J. Haidn. "Experimental and Numerical Investigation of CH$$_4$$/O$$_2$$ Rocket Combustors." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 359–79. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_23.
Повний текст джерелаDecher, Reiner. "More Components: Inlets, Mixers, and Nozzles." In The Vortex and The Jet, 137–54. Singapore: Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_13.
Повний текст джерелаAkhmedzyanov, D. A., and A. E. Kishalov. "Computer-Aided Design and Construction Development of the Main Elements of Aviation Engines." In Lecture Notes in Electrical Engineering, 693–702. Cham: Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-39225-3_76.
Повний текст джерелаТези доповідей конференцій з теми "Rocket engines – Design and construction"
Kobald, M., C. Schmierer, U. Fischer, K. Tomilin, A. Petrarolo, and M. Rehberger. "The HyEnD stern hybrid sounding rocket project." In Progress in Propulsion Physics – Volume 11. Les Ulis, France: EDP Sciences, 2019. http://dx.doi.org/10.1051/eucass/201911025.
Повний текст джерелаSAGER, PAUL. "Design considerations in clustering nuclear rocket engines." In 28th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3587.
Повний текст джерелаGUNN, STAN. "Design of second-generation nuclear thermal rocket engines." In 26th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-1954.
Повний текст джерелаSmith, Nathan. "Facility design and testing of micro-hybrid rocket engines." In 39th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-5.
Повний текст джерелаCasalino, Lorenzo, Filippo Masseni, and Dario Pastrone. "Comparison of Robust Design Approaches for Hybrid Rocket Engines." In 53rd AIAA/SAE/ASEE Joint Propulsion Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-4642.
Повний текст джерелаHUYNH, C., A. GHAFOURIAN, S. MAHALINGAM, and J. DAILY. "Combustor design for atomization study in liquid rocket engines." In 30th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-465.
Повний текст джерелаCasalino, Lorenzo, Filippo Masseni, and Dario Pastrone. "Uncertainty Analysis and Robust Design for Hybrid Rocket Engines." In 2018 Joint Propulsion Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-4839.
Повний текст джерелаRaghavan, Madhusudan. "The Variable Rocker-Arm Mechanism." In ASME 2005 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2005. http://dx.doi.org/10.1115/detc2005-85150.
Повний текст джерелаMEYER, MICHAEL. "Design issues for lunar in situ aluminum/oxygen propellant rocket engines." In Aerospace Design Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-1185.
Повний текст джерелаLIMERICK, C. "Component design concerns for deep throttling H2/O2 rocket engines." In 27th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-2209.
Повний текст джерелаЗвіти організацій з теми "Rocket engines – Design and construction"
Morais, Carla, António Coelho, Alexandre Jacinto, and Marta Varzim, eds. The I SEA Project: Digital Publications. Faculdade de Ciências da Universidade do Porto, October 2020. http://dx.doi.org/10.24840/2020/978-989-746-279-5.
Повний текст джерела