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25 kW power module evolution studyThis paper presents a study of evolutionary growth concepts for the 25 kW power module to augment STS mission support future capabilities. The study aimed to establish user payload requirements, define evolution methods for system initial operational capability, and formulate a development program and conceptual designs. The payload requirements analysis focused on material processing in space, public services, and solar terrestrial observations; evolutionary system concepts were evaluated to derive the power module and system support requirements, and four reference orbits were used to construct the nominal program scenario. The mission accomodations analysis evaluated the capability of the nominal program scenario and associated power module concepts to meet user needs. Finally, the recommended modular design consisting of electric power, attitude control, thermal control, and command and data handling is described, and it is concluded that the 25 kW power module is a logical first step to support the near term NASA sortie and free-flyer mission requirements.
Document ID
19790067883
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Overall, J. W., Jr.
(Lockheed Missiles and Space Co., Inc. Space Systems Div., Sunnyvale, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: Intersociety Energy Conversion Engineering Conference
Location: Boston, MA
Start Date: August 5, 1979
End Date: August 10, 1979
Accession Number
79A51896
Distribution Limits
Public
Copyright
Other

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