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Beyond Aerobraking: Designing the Magellan Global Gravity ExperimentThe orbit of the Magellan spacecraft was circularized during a 70 day aerobraking phase, which ended on August 3, 1993. Shrinking the orbit apoapsis from 8467 km down to 541 km was required to obtain meaningful gravity science data at high and moderate latitudes. Aerobraking was the only way to reach this nearly-circular orbit, since the amount of propellant on board Magellan was at least an order of magnitude too small to circularize propulsively. This paper will describe the gravity science experiment which drove the final design of the nearly-circular orbit. Magellan is currently in a 541 by 197 km altitude orbit around the planet Venus. This paper will also briefly describe the Magellan mission history, and then describe the design tradeoffs which went into picking the desired nearly-circular orbit.
Document ID
20210004602
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
Authors
Austin, Rick S.
Lock, Robert E.
Sjogren, William L.
Lyons, Daniel T.
Date Acquired
August 1, 1993
Publication Date
August 1, 1993
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review

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