Results 1 to 10 of about 410,560 (293)
Design and Simulation of Single Capillary Injector and Circular Injector Plate for a Monopropellant Thruster [PDF]
فصلنامه علوم و فناوری فضایی, 2022 In this research, design and simulation of a single capillary injector and three-hole circular injector plate of a 10N Hydrazine monopropellant thruster were performed. Ansys Fluent software was used to simulate the injector and injector plate .
Sajad Davari, Hadiseh Karimaei
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Aerospace, 2023 This paper explores the use of the averaging method in the optimal control problem related to the multirevolution orbital transfer of a spacecraft with low-thrust capabilities.
Kirill Suslov +2 more
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Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2023 A digital model is described for estimating the drag force of the Earth's upper atmosphere acting on a low-orbit spacecraft. Unlike the classical model of aerodynamic force, the digital model is the result of a computer algorithm.
V. V. Volotsuev
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Low-thrust perturbation guidance [PDF]
Astrodynamics Conference, 1982 Low-thrust perturbation guidance, as applied to the minimum time problem of an Earth to Mars rendezvous, has been reexamined and shown to perform orders of magnitude better, as measured by the terminal state error, than previous studies indicated. The orbits of Earth and Mars were assumed to be inclined and elliptical.
T. BAUER, L. WOOD, T. CAUGHEY
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Provide a Predictive Model for the Preliminary Design of Swirl Injectors Based on Neuro-Fuzzy Model Thruster [PDF]
فصلنامه علوم و فناوری فضایی, 2019 the effect of the internal geometry of the injector of a low-thrust monopropellant thruster on the characteristics of the outlet liquid sheet, such as the liquid sheet thickness, the spray cone angle, the average output velocity, and its mass flow rate ...
Hadiseh Karimaei
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Autonomous Optimal Absolute Orbit Keeping through Formation Flying Techniques
Aerospace, 2023 In this paper, the problem of autonomous optimal absolute orbit keeping for a satellite mission in Low Earth Orbit using electric propulsion is considered.
Ahmed Mahfouz +3 more
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Impact of basement thrust faults on low-angle normal faults and rift basin evolution: a case study in the Enping sag, Pearl River Basin [PDF]
Solid Earth, 2021 Reactivation of pre-existing structures and their influence on subsequent rift evolution have been extensively analysed in previous research on rifts that experienced multiple phases of rifting, where pre-existing structures were deemed to affect ...
C. Deng +7 more
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Automation of low-thrust engine testing
Космические аппараты и технологии, 2023 The article discusses the key role of the use of automation in the stands, as well as the ignition system of the stand of low-thrust engines and the features of its operation as part of the stand.
A. D. Shirokov +4 more
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Results in Engineering, 2023 A growing number of space missions use electric propulsion systems due to their higher specific impulse and greater efficiency compared to chemical propulsion systems.
Ugur Kokal, Emin Saridede, Murat Celik
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Simulation and Experiment of Ionic Wind Thruster at Low Air Pressures
气体物理, 2023 Thrust generated by ionic wind has the advantages of no mechanical rotating parts, low power consumption and low noise, and has important application potential in stratospheric airships and solar planes.
Rong-hui QUAN, Bo WANG, Yun-jia YAO
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