The feasibility of developing a solar electric multimission spacecraft (SEMMS) is examined with emphasis on understanding the effect of solar electric propulsion elements on a spacecraft system design. The applicability of Mariner, Viking, and thermoelectric outer planet spacecraft (TOPS) technologies to postulated mission/science objectives is investigated. A Mariner/Viking-based, modular spacecraft evolves which, with minimum modifications, is capable of performing a variety of interplanetary missions, including comet and asteroid rendezvous and orbit of Mercury, Jupiter, and Saturn. An early technology-evaluation flight is recommended to minimize the risk in subsequent missions.
SEMMS - Understanding the solar electric multimission concept.
American Institute of Aeronautics and Astronautics, Electric Propulsion Conference ; 1972 ; Bethesda, MD
01.04.1972
Aufsatz (Konferenz)
Keine Angabe
Englisch
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