NASA NTRS · 19880059262
Advanced propulsion for the Mars Rover Sample Return Mission
Abstract
The present evaluation of highly detailed advanced propulsion system design concepts for the Mars Rover Sample Return Mission proceeded by comparing a baseline chemical propulsion option with both storable and cryogenic advanced chemical propulsion alternatives and solar- and nuclear-based electric propulsion OTVs. Substantial launch mass reductions and commensurate payload mass increases were obtainable with both advanced chemical and electric propulsion cycles.
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Palaszewski, Bryan, Frisbee, Robert. 1988-07-01. Advanced propulsion for the Mars Rover Sample Return Mission. https://ntrs.nasa.gov/citations/19880059262
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