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Flight performance of the High Energy Astronomy Observatory /HEAO 1/ power subsystemThe design and flight performance of the HEAO-1 power subsystem is described. Solar array power analysis and test data are compared to orbital performance. The batteries are described along with parametric cell tests which led to the temperature-compensated voltage limits used in the charge controls. Battery life test results, used for verification of battery charger temperature-compensated voltage limits, are compared with orbital performance. The control electronics are
Document ID
19790025989
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Reppucci, G. M. (TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Schulman, I. M. (TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Wright, W. H. (TRW Defense and Space Systems Group Redondo Beach, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Intersociety Energy Conversion Engineering Conference
Location: San Diego, CA
Start Date: August 20, 1978
End Date: August 25, 1978
Accession Number
79A10002
Funding Number(s)
CONTRACT_GRANT: NAS8-28300
Distribution Limits
Public
Copyright
Other

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