Charged Particle Electrostatic Thrusters.
Technical rept. 15 Aug 67-15 Dec 68,
TRW SYSTEMS GROUP REDONDO BEACH CA
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This program was directed toward the demonstration of long-term efficient electrostatic engine operation in the 1000-second specific impulse range. The state of the art in this performance range has been advanced to where practical flight system design is feasible. Author
- Electric and Ion Propulsion