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An orbital service module systems conceptAn Orbital Service Module (OSM) system represents a concept for an evolutionary program that will provide utilities services such as electrical power, heat rejection, attitude control, and communications to support payload operations in both Shuttle-tended and untended (free-flyer) modes. The initial program step is a Space Transportation System (STS) power extension package (a solar array system carried by the Orbiter and deployed by the remote manipulator system). The power extension package (PEP) develops the major components of the more sophisticated OSM vehicles. Major objectives of such an approach are (1) the continuous matching of a capability to meet real needs while avoiding the pitfalls usually associated with the uncertainties inherent in long-range prediction of future requirements, and (2) the economies attendant with program continuity and hardware commonality. The initial Orbiter-carried PEP and several later OSM system growth options are discussed.
Document ID
19780068832
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Craig, J. W.
(NASA Johnson Space Center Technical Planning Office, Houston, Tex., United States)
Daros, C. J.
(McDonnell Douglas Astronautics Co. Huntington Beach, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
September 1, 1978
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
AIAA PAPER 78-1694
Accession Number
78A52741
Distribution Limits
Public
Copyright
Other

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