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Space hardware designs, volume 1The design of a solar sail space vehicle with a novel sail deployment mechanism is described. The sail is triangular in shape and is deployed and stabilized by three miniature spacecraft, one at each corner of the triangle. A concept demonstrator for a spherical microrover for the exploration of a planetary surface is described. Lastly, laboratory experiments have been conducted to study the migration of thin oil films on metal surfaces in the presence of a thermal gradient.
Document ID
19950006250
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Meyer, Rudolf X.
(California Univ. Los Angeles, CA, United States)
Cribbs, Richard
(California Univ. Los Angeles, CA, United States)
Honda, Mark
(California Univ. Los Angeles, CA, United States)
Ma, Christina
(California Univ. Los Angeles, CA, United States)
Robson, Christopher
(California Univ. Los Angeles, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1994
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.26:197209
NASA-CR-197209
Report Number: NAS 1.26:197209
Report Number: NASA-CR-197209
Accession Number
95N12663
Funding Number(s)
CONTRACT_GRANT: NASW-4435
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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