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- W587649002 abstract "Current analysis of advanced unmanned planetary missions in the 1980's and beyond indicate the need for propulsion systems with performance capabilities beyond those of current and near state-of-art. One propulsion system concept being considered to fill this need is nuclear electric low thrust propulsion (NEP). Two different NEP system power levels are considered for performance analysis: 100 kw and 250 kw. The 100 kw NEP system uses a Centaur(D-1T) chemical stage for injection to an interplanetary transfer and the 250 kw system uses a spiral escape maneuver. Performance comparison is in general made on the basis of net payload at the target as a function of flight time. NEP performance is shown for unconstrained and constrained (20,000 hours) thrusting time. Specific impulse is optimized and ranges from 4000 sec to 7000 sec." @default.
- W587649002 created "2016-06-24" @default.
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- W587649002 date "1972-07-01" @default.
- W587649002 modified "2023-09-27" @default.
- W587649002 title "Advanced mission applications of nuclear electric propulsion" @default.
- W587649002 hasPublicationYear "1972" @default.
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