Статті в журналах з теми "Rocket engines – Design and construction"
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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 джерелаSzwaja, Stanisław, and Mirosław Szymkowiak. "The Szymkowiak’s over-expanded cycle in the rocker engine with the variable compression ratio – kinematics." Combustion Engines 189, no. 2 (October 30, 2021): 68–72. http://dx.doi.org/10.19206/ce-143157.
Повний текст джерелаСалич, В. Л. "A numerical study of the working process in the chamber of a thruster rocket engine based on oxygen-hydrogen fuel." Numerical Methods and Programming (Vychislitel'nye Metody i Programmirovanie), no. 2 (June 30, 2015): 187–95. http://dx.doi.org/10.26089/nummet.v16r219.
Повний текст джерелаPartola, I. S. "Design of liquid-propellant rocket engines." Journal of Machinery Manufacture and Reliability 41, no. 6 (November 2012): 492–98. http://dx.doi.org/10.3103/s1052618812060118.
Повний текст джерелаKamennov, P. B. "PRC’S MILITARY-INDUSTRIAL COMPLEX UNDER XI JINPING." Outlines of global transformations: politics, economics, law 10, no. 5 (December 20, 2017): 135–51. http://dx.doi.org/10.23932/2542-0240-2017-10-5-135-151.
Повний текст джерелаRyzhkov, V. V. "The structure of knowledge base to support the development of low-thrust liquid-propellant rocket engines based on computer technologies." VESTNIK of Samara University. Aerospace and Mechanical Engineering 20, no. 4 (January 19, 2022): 28–39. http://dx.doi.org/10.18287/2541-7533-2021-20-4-28-39.
Повний текст джерелаShulga, V. A., and A. V. Dibrivny. "Design Office of Liquid Rocket Engines is 60." Kosmičeskaâ tehnika. Raketnoe vooruženie 2018, no. 2 (September 14, 2018): 3–7. http://dx.doi.org/10.33136/stma2018.02.003.
Повний текст джерелаRay, A., M. S. Holmes, and C. F. Lorenzo. "Life extending controller design for reusable rocket engines." Aeronautical Journal 105, no. 1048 (June 2001): 315–22. http://dx.doi.org/10.1017/s0001924000012197.
Повний текст джерелаEtele, J., T. Waung, and D. J. Cerantola. "Exchange Inlet Design for Rocket-Based Combined-Cycle Engines." Journal of Propulsion and Power 28, no. 5 (September 2012): 1026–36. http://dx.doi.org/10.2514/1.b34531.
Повний текст джерелаLee, Dae-Sung, Chang-Ho Choi, Jin-Han Kim, and Soo-Seok Yang. "Design of a Turbine System for Liquid Rocket Engines." Journal of Fluid Machinery 5, no. 4 (December 1, 2002): 11–18. http://dx.doi.org/10.5293/kfma.2002.5.4.011.
Повний текст джерелаBasharina, T. A., M. G. Goncharov, S. N. Lymich, V. S. Levin, and D. P. Shmatov. "Low-thrust liquid-propellant rocket engines as part of advanced ultralight rocket vehicle systems." Spacecrafts & Technologies 5, no. 1 (March 25, 2021): 5–13. http://dx.doi.org/10.26732/j.st.2021.1.01.
Повний текст джерелаSiva Vasanth, A., J. Stalin, and A. Benzigar Rajan. "Instrumentation design considerations for automatic ground testing of rocket engines." Indian Journal of Cryogenics 46, no. 1 (2021): 171–77. http://dx.doi.org/10.5958/2349-2120.2021.00030.3.
Повний текст джерелаSantana Jr., A., M. S. Silva, P. T. Lacava, and L. C. S. Góes. "ACOUSTIC CAVITIES DESIGN PROCEDURES." Revista de Engenharia Térmica 6, no. 2 (December 31, 2007): 27. http://dx.doi.org/10.5380/reterm.v6i2.61687.
Повний текст джерелаGuo, Feng, Wenguo Luo, Feng Gui, Jianfeng Zhu, Yancheng You, and Fei Xing. "Efficiency Analysis and Integrated Design of Rocket-Augmented Turbine-Based Combined Cycle Engines with Trajectory Optimization." Energies 13, no. 11 (June 5, 2020): 2911. http://dx.doi.org/10.3390/en13112911.
Повний текст джерелаCasalino, Lorenzo, Andrea Ferrero, Filippo Masseni, and Dario Pastrone. "Emission-Driven Hybrid Rocket Engine Optimization for Small Launchers." Aerospace 9, no. 12 (December 9, 2022): 807. http://dx.doi.org/10.3390/aerospace9120807.
Повний текст джерелаGlebov, G. A., and S. A. Vysotskaya. "On the question of solid-propellant rocket engine design preventing unstable operation in the combustion chamber." Journal of «Almaz – Antey» Air and Space Defence Corporation, no. 4 (December 30, 2017): 63–72. http://dx.doi.org/10.38013/2542-0542-2017-4-63-72.
Повний текст джерелаSon, Min, Kanmaniraja Radhakrishnan, Jaye Koo, Oh Chae Kwon, and Heuy Dong Kim. "Design Procedure of a Movable Pintle Injector for Liquid Rocket Engines." Journal of Propulsion and Power 33, no. 4 (July 2017): 858–69. http://dx.doi.org/10.2514/1.b36301.
Повний текст джерелаKonokh, V. I., V. S. Boiko, A. B. Troyak, and A. V. Ivashura. "Electromagnetic Valves Developed by Yuzhnoye SDO Liquid Rocket Engines Design Office." Kosmičeskaâ tehnika. Raketnoe vooruženie 2018, no. 2 (September 14, 2018): 34–48. http://dx.doi.org/10.33136/stma2018.02.034.
Повний текст джерелаKANDA, Takeshi, Yohei OGAWA, Daizo SUGIMORI, and Makoto KOJIMA. "Conceptual Design Model of High-Altitude Test Stand for Rocket Engines." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 59, no. 3 (2016): 161–69. http://dx.doi.org/10.2322/tjsass.59.161.
Повний текст джерелаRamesh, Davood, Hasan Karimi M., and Massoud Shahheidari. "Cycle optimization of the staged combustion rocket engines." Aircraft Engineering and Aerospace Technology 89, no. 2 (March 6, 2017): 304–13. http://dx.doi.org/10.1108/aeat-12-2013-0229.
Повний текст джерелаLiu, Chao Ying, and Ran Duan. ""A+T·CDIO"-Architecture Major Oriented Talents Cultivation Objectives Establishment and Curriculum System Construction - Using Architecture Major of Ningbo University of Technology as Example." Applied Mechanics and Materials 357-360 (August 2013): 2806–9. http://dx.doi.org/10.4028/www.scientific.net/amm.357-360.2806.
Повний текст джерелаAnoop, C. R., John Bejoy, Thomas Tharian, and P. V. Venkitakrishnan. "Evaluation of Mechanical Properties of the Rocket Thrust Chamber Material under Flight Conditions." Materials Science Forum 830-831 (September 2015): 219–22. http://dx.doi.org/10.4028/www.scientific.net/msf.830-831.219.
Повний текст джерелаKang, Sang Hun, and Jesun Jang. "Design and Hot Fire Tests of the Pyrostarter for Liquid Rocket Engines." Journal of the Korean Society of Propulsion Engineers 18, no. 3 (June 1, 2014): 48–55. http://dx.doi.org/10.6108/kspe.2014.18.3.048.
Повний текст джерелаElkin, Andrey. "Rocket engines for spacecraft on fluidized solid propellants, their design and thermodynamics." Thermal processes in engineering 13, no. 11 (2021): 509–18. http://dx.doi.org/10.34759/tpt-2021-13-11-509-518.
Повний текст джерелаRyzhkov, V. V., I. I. Morozov, and E. A. Lapshin. "Computer-aided design of low-thust rocket engines using the domain-specific knowledge database and CAE / CAD systems." VESTNIK of Samara University. Aerospace and Mechanical Engineering 18, no. 4 (January 21, 2020): 106–16. http://dx.doi.org/10.18287/2541-7533-2019-18-4-106-116.
Повний текст джерелаMessineo, Jérôme, and Toru Shimada. "Theoretical Investigation on Feedback Control of Hybrid Rocket Engines." Aerospace 6, no. 6 (June 3, 2019): 65. http://dx.doi.org/10.3390/aerospace6060065.
Повний текст джерелаVaulin, S. D., and K. I. Khazhiakhmetov. "The State-of-the-Art and Prospects of Aerospike Engines." Proceedings of Higher Educational Institutions. Маchine Building, no. 10 (739) (October 2021): 74–83. http://dx.doi.org/10.18698/0536-1044-2021-10-74-83.
Повний текст джерелаLamb, Thomas, Alex M. Loudon, and Robert J. Van Slyke. "The Lockheed Space Shuttle Rocket Retrieval Ship." Marine Technology and SNAME News 23, no. 02 (April 1, 1986): 109–22. http://dx.doi.org/10.5957/mt1.1986.23.2.109.
Повний текст джерелаRugescu, Radu Dan, Florin Radu Bacaran, and Stefan Catalin Predoiu. "Starting Transient Experiments in the MEC-80 Rocket Engine Scaled Ignition Device." Applied Mechanics and Materials 656 (October 2014): 110–17. http://dx.doi.org/10.4028/www.scientific.net/amm.656.110.
Повний текст джерелаKim, Hye In, Tae-Seong Roh, Hwanil Huh, and Hyoung Jin Lee. "Development of Ultra-Low Specific Speed Centrifugal Pumps Design Method for Small Liquid Rocket Engines." Aerospace 9, no. 9 (August 28, 2022): 477. http://dx.doi.org/10.3390/aerospace9090477.
Повний текст джерелаKhan, Suniya Sadullah, Ihtzaz Qamar, Muhammad Umer Sohail, Raees Fida Swati, Muhammad Azeem Ahmad, and Saad Riffat Qureshi. "Comparison of Optimization Techniques and Objective Functions Using Gas Generator and Staged Combustion LPRE Cycles." Applied Sciences 12, no. 20 (October 17, 2022): 10462. http://dx.doi.org/10.3390/app122010462.
Повний текст джерелаRazin, A. F. "The Problem of Optimum Design of Composite Housings of Solid Propellant Rocket Engines." Mechanics of Solids 53, no. 4 (July 2018): 418–26. http://dx.doi.org/10.3103/s0025654418040076.
Повний текст джерелаRyzhkov, V., and E. Lapshin. "Computer Design Technology of the Small Thrust Rocket Engines Using CAE / CAD Systems." IOP Conference Series: Materials Science and Engineering 302 (January 2018): 012032. http://dx.doi.org/10.1088/1757-899x/302/1/012032.
Повний текст джерелаFrank, Christopher P., Olivia J. Pinon-Fischer, Dimitri N. Mavris, and Clémence M. Tyl. "Design Methodology for the Performance, Weight, and Economic Assessment of Chemical Rocket Engines." Journal of Aerospace Engineering 30, no. 1 (January 2017): 04016071. http://dx.doi.org/10.1061/(asce)as.1943-5525.0000668.
Повний текст джерелаЛавров, С. В., and Б. К. Терпогосова. "CHOOSING RATIONAL ENGINEERING SOLUTIONS AND DESIGN CRITERIA OF THROTTABLE SOLID FUEL ROCKET ENGINES." Южно-Сибирский научный вестник, no. 5(45) (October 31, 2022): 78–81. http://dx.doi.org/10.25699/sssb.2022.45.5.010.
Повний текст джерелаCasalino, Lorenzo, Filippo Masseni, and Dario Pastrone. "Hybrid Rocket Engine Design Optimization at Politecnico di Torino: A Review." Aerospace 8, no. 8 (August 13, 2021): 226. http://dx.doi.org/10.3390/aerospace8080226.
Повний текст джерелаAsraff, A. K., S. Sheela, Krishnajith Jayamani, S. Sarath Chandran Nair, and R. Muthukumar. "Material Characterisation and Constitutive Modelling of a Copper Alloy and Stainless Steel at Cryogenic and Elevated Temperatures." Materials Science Forum 830-831 (September 2015): 242–45. http://dx.doi.org/10.4028/www.scientific.net/msf.830-831.242.
Повний текст джерелаNae, Catalin, Irina-Carmen Andrei, Gabriela-Liliana Stroe, and Sorin Berbente. "Integration of Fuels Types and Chemical Properties with the Design of the Rocket Engine�s Bell Exhaust Nozzle and Combustion Chamber." Revista de Chimie 71, no. 1 (February 7, 2020): 436–44. http://dx.doi.org/10.37358/rc.20.1.7872.
Повний текст джерелаPonomarov, O. M., O. O. Dobrodomov, and O. V. Kulyk. "Prospects for the use of nitrogen-containing single-component rocket propellants." Technical mechanics 2022, no. 3 (October 3, 2022): 85–90. http://dx.doi.org/10.15407/itm2022.03.085.
Повний текст джерелаZapata Usandivaras, José Felix, Annafederica Urbano, Michael Bauerheim, and Bénédicte Cuenot. "Data Driven Models for the Design of Rocket Injector Elements." Aerospace 9, no. 10 (October 12, 2022): 594. http://dx.doi.org/10.3390/aerospace9100594.
Повний текст джерелаAbada, Omar, Abderahim Abada, and Ahmed Abdallah El-Hirtsi. "Effect of bipropellant combustion products on the rocket nozzle design." Mechanics & Industry 21, no. 5 (2020): 515. http://dx.doi.org/10.1051/meca/2020064.
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