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)