This paper details the objectives of the mission, the key constraints that influenced the mission design, and the flight and ground system implementation. Issues that influenced the mission architecture are discussed, as well as the technology assumptions.
A fission powered Mars Telecommunications Orbiter mission concept
2003-02-02
Miscellaneous
No indication
English
fission , nuclear , propulsion , optical , communication , power , electric , space
A Fission Powered Mars Telecommunications Orbiter Mission Concept
British Library Conference Proceedings | 2003
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