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Power, thermal, and attitude control design interactions of the CCE/AMPTE spacecraftThe power, thermal and attitude control interactions of the CCE spacecraft and the design compromises resulting from these interactions are described. These compromises result from the conflict between the plane change maneuver requirements and the final on station requirements. The resolution of these conflicts to arrive at an acceptable final design, is given and the resulting power, thermal and attitude control systems are described in some detail.
Document ID
19820063451
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wingate, C. A., Jr.
(Johns Hopkins Univ. Silver Spring, MD, United States)
Allen, W. E.
(Johns Hopkins Univ. Silver Spring, MD, United States)
Smola, J. F.
(Johns Hopkins Univ. Silver Spring, MD, United States)
Ray, J. C.
(Johns Hopkins University Applied Physics Laboratory, Laurel, MD, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
IAF PAPER 82-200
Accession Number
82A46986
Funding Number(s)
CONTRACT_GRANT: N0024-81-C-5301
Distribution Limits
Public
Copyright
Other

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