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- W242838342 abstract "The purpose of the spacecraft is to space qualify a number of components for the next generation of communications satellites. The state of development of ion thrusters has reached a point where at least three types of engine may be considered for integration on spacecraft. The proposed methods of stationkeeping require that the thruster operate with a duty cycle of somewhat less than 12 hours in a 24 hour period. Several possible mounting positions for the thrusters were considered during the conceptual design phase. It is concluded that an experimental ion thruster subsystem may be incorporated in the communication satellite and used to demonstrate, at a minimum, north-south stationkeeping of the spacecraft in synchronous orbit." @default.
- W242838342 created "2016-06-24" @default.
- W242838342 date "1972-04-17" @default.
- W242838342 modified "2023-09-25" @default.
- W242838342 title "Choice of an ion engine for the Communications Technology Satellite" @default.
- W242838342 doi "https://doi.org/10.2514/6.1972-491" @default.
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