NASA NTRS · 19640041237
Optimum earth-to-mars roundtrip trajectories utilizing a low-thrust power-limited propulsion system.
Abstract
Payload capabilities of low thrust power limited spacecraft for earth to mars round trip trajectories
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Melbourne, W. G., Sauer, C. G., Jr.. 1964-01-01. Optimum earth-to-mars roundtrip trajectories utilizing a low-thrust power-limited propulsion system.. https://ntrs.nasa.gov/citations/19640041237
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