Optimum earth-to-mars roundtrip trajectories utilizing a low-thrust power-limited propulsion system.

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Optimum earth-to-mars roundtrip trajectories utilizing a low-thrust power-limited propulsion system.

Optimum earth-to-mars roundtrip trajectories utilizing a low-thrust power-limited propulsion system.

Melbourne, W. G. / Sauer, C. G., Jr.

Payload capabilities of low thrust power limited spacecraft for earth to mars round trip trajectories

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Title :

Optimum earth-to-mars roundtrip trajectories utilizing a low-thrust power-limited propulsion system.

Contributors:

Melbourne, W. G. (author) / Sauer, C. G., Jr. (author)

Publication date :

1964-01-01

Type of media :

Conference paper

Type of material :

No indication

Language :

English

Keywords :

SPACECRAFT TRAJECTORY , Space Radiation , ORBITAL TRANSFER , ROUND-TRIP TRAJECTORY

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