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MSFC Skylab electrical power systems mission evaluationThe design, development, and operation of the Skylab electrical power system are discussed. The electrical systems for the airlock module of the orbital workshop and the Apollo telescope mount are described. Skylab is considered an integral laboratory, however, both cluster and module hardware distinct sections are included. Significant concept and requirement evolution, testing, and modifications resulting from tests are briefly summarized to aid in understanding the launch configuration description and the procedures and performance discussed for in-orbit operation. Specific problems encountered during Skylab orbital missions are analyzed.
Document ID
19740022202
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Woosley, A. P. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1974
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-64818
Accession Number
74N30315
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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