Development of a PPT for the EO-1 Spacecraft
作者： Scott Benson , Lynn Arrington , W. Hoskins , Nicole Meckel
DOI: 10.2514/6.1999-2276
关键词: Automotive engineering 、 Aerospace engineering 、 Specific impulse 、 Spacecraft 、 Electrically powered spacecraft propulsion 、 Attitude control 、 Acceptance testing 、 Spacecraft propulsion 、 Engineering 、 Pulsed plasma thruster 、 Reaction wheel
摘要: … A Pulsed Plasma Thruster (PPT) has been developed for use in a … The EO-1 PPT configuration is a combination of new … This paper reviews the EO-1 PPT development, including …
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