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Sensor deployment mechanism for Surfer satelliteA design is presented for a sensor-deployment mechanism to be used aboard the Surfer satellite, from which scientific instruments will be extended to study the earth ionosphere during the Space Shuttle Tether Experiment. The design discussed uses four folding arms to extend the radial sensors, as well as two storable tubular extendible members or spirally wound self-extending tube booms to project the axial sensors outward. The design solution chosen, a folding arm, is discussed in detail with attention to mechanical operation and component functions. Test program results are presented.
Document ID
19900055191
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dill, Robert
(Stanford Univ. CA, United States)
Flom, James
(Stanford Univ. CA, United States)
Gibbons, Donald
(Stanford University CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90A42246
Funding Number(s)
CONTRACT_GRANT: NCA2-308
Distribution Limits
Public
Copyright
Other

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