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Transient Plume Model Testing Using LADEE Spacecraft Attitude Control System OperationsThe Lunar Atmosphere Dust Environment Explorer (LADEE) spacecraft is being designed for a mission featuring low altitude orbits of the Moon to take relevant ambient measurements before that environment becomes altered by future exploration activities. Instruments include a neutral mass spectrometer capable of measuring ambient species density levels below 100 molecules/cu cm. Coincidentally, with a favorable combination of spacecraft orientations, it is also possible to measure plume gases from LADEE attitude control system thruster operations as they are reflected from the daytime lunar surface and subsequently intercepted by the spacecraft as it orbits overhead. Under such circumstances, it may be possible to test a variety of properties and assumptions associated with various transient plume models or to infer certain aspects regarding lunar surface properties.
Document ID
20100026430
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Woronowicz, M. S.
(Stinger Ghaffarian Technologies, Inc. (SGT, Inc.) Greenbelt, MD, United States)
Date Acquired
August 24, 2013
Publication Date
July 10, 2010
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Rarefied Gas Dynamics Conference
Location: Pacific Grove, CA
Country: United States
Start Date: July 10, 2010
End Date: July 15, 2010
Funding Number(s)
CONTRACT_GRANT: NNG07CA21C
Distribution Limits
Public
Copyright
Public Use Permitted.
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