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Standard power regulator for the multi-mission modular spacecraftThe Standard Power Regulator Unit (SPRU) which forms the central building block of the Modular Power Subsystem (MPS) for the Multi-mission Modular Spacecraft (MMS) is described. A functional description of the SPRU is presented, detailing key design features, operational characteristics, and internal redundancy as well as giving block and schematic diagrams for all major subassemblies. The description of a qualification test program consisting of ten sequences ranging from a physical examination of the unit to calculating vibration and sine sweep of power on shock tests is presented. The results showed that some significant anomalies were encountered but no catastrophic failures were indicated, although several power module failures were found due to overvoltage malfunctions of the solar array stimulator.
Document ID
19790067906
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Kichak, R. A.
(NASA Goddard Space Flight Center Spacecraft Technology Div., Greenbelt, Md., 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
79A51919
Distribution Limits
Public
Copyright
Other

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