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Three-Axis Attitude Control for Solar-Powered Electric Propulsion Spacecraft
SAE Technical Paper Series, 1974Spacecraft utilizing solar electric propulsion (SEP) for certain long-term interplanetary missions will depend on large, flexible solar arrays. The resulting spacecraft configurations present some complex flight control problems. Questions regarding a general design approach are discussed along with options for three-axis control forces, tradeoffs for
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A Spacecraft Electric Propulsion System Using Hybrid Excitation Generator for Deep Space Missions
IEEE Aerospace ConferenceThis study presents an in-space nuclear electric propulsion system integrating a multiphase hybrid excitation generator. In spite of the low amount of thrust of electric thrusters, their high specific impulse, high efficiency and constant thrust make ...
Mahzad Gholamian+3 more
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Space engineering and technology, 2019
The article summarizes the results of a 15-year operation of the Yamal-202 telecommunication spacecraft in geostationary orbit. The review of using electrical rocket engines in spacecraft in domestic and foreign projects is made.
Vladimir N. Bashmakov+7 more
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The article summarizes the results of a 15-year operation of the Yamal-202 telecommunication spacecraft in geostationary orbit. The review of using electrical rocket engines in spacecraft in domestic and foreign projects is made.
Vladimir N. Bashmakov+7 more
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Review of electric rocket engines for small spacecraft propulsion systems
Omsk Scientific Bulletin Series Aviation-Rocket and Power EngineeringThe article analyzes the current state of global development of low-energy plasma propulsion systems for guided small spacecraft. The aim of the research is to review the main types and constructions of electric rocket engines, to identify the problems ...
I. V. Kolganov
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1966
Abstract Advanced scientific missions throughout the solar system are analyzed to determine payload and velocity requirements for nuclear-electric propelled spacecraft. Emphasis is placed upon those missions that are too difficult for all-chemical propulsion, even with boosters as large as Saturn V.
H. Brown, T.F. Widmer
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Abstract Advanced scientific missions throughout the solar system are analyzed to determine payload and velocity requirements for nuclear-electric propelled spacecraft. Emphasis is placed upon those missions that are too difficult for all-chemical propulsion, even with boosters as large as Saturn V.
H. Brown, T.F. Widmer
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Herald of Aeroenginebuilding, 2017
Рассмотрена интегрированная в состав космического аппарата (КА) система его увода с низких околоземных и геостационарной орбит на безопасные в случае аварии или после окончания срока активного существования КА, работа которой основана на применении электроракетных двигателей (ЭРД).
Dron’, N.M.+2 more
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Рассмотрена интегрированная в состав космического аппарата (КА) система его увода с низких околоземных и геостационарной орбит на безопасные в случае аварии или после окончания срока активного существования КА, работа которой основана на применении электроракетных двигателей (ЭРД).
Dron’, N.M.+2 more
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2024 3rd Asian Conference on Frontiers of Power and Energy (ACFPE)
As one of the primary power sources for deep space propulsion, scholars have extensively researched electrical energy. The utilization of electrical energy in deep space predominantly relies on electric thrusters, and propellant, as one of the ...
Xinyu Liu+3 more
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As one of the primary power sources for deep space propulsion, scholars have extensively researched electrical energy. The utilization of electrical energy in deep space predominantly relies on electric thrusters, and propellant, as one of the ...
Xinyu Liu+3 more
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Advanced rocket propulsion techniques for deep space travel: A review
IEEE Conference on Computer Communications, 2017Swaraj Singh+3 more
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Design of Deep Space Electric Propulsion Spacecraft Power System
2023 6th International Conference on Energy, Electrical and Power Engineering (CEEPE), 2023Yingjun Lei, Yue Han, Yi Yang
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Power Processing Unit and Feed System Development for a Multimode Spacecraft Propulsion System
AIAA Propulsion and Energy 2021 Forum, 2021Jacob Eisen+3 more
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