NASA NTRS · 19710027901
Thermionic spacecraft design study, 120 kw nuclear electric propulsion system. Volume 1: Summary
Abstract
Electrically propelled spacecraft designs using thermionic reactors as electrical power source investigated for Halley Comet rendezvous mission
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1971-06-30. Thermionic spacecraft design study, 120 kw nuclear electric propulsion system. Volume 1: Summary. https://ntrs.nasa.gov/citations/19710027901
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