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Space station thermal control surfaces. Volume 1: Interim reportThe U.S. space program goals for long-duration manned missions place particular demands on thermal-control systems. The objective of this program is to develop plans which are based on the present thermal-control technology, and which will keep pace with the other space program elements. The program tasks are as follows: (1) requirements analysis, with the objectives to define the thermal-control-surface requirements for both space station and 25 kW power module, to analyze the missions, and to determine the thermal-control-surface technology needed to satisfy both sets of requirements; (2) technology assessment, with the objectives to perform a literature/industry survey on thermal-control surfaces, to compare current technology with the requirements developed in the first task, and to determine what technology advancements are required for both the space station and the 25 kW power module; and (3) program planning that defines new initiative and/or program augmentation for development and testing areas required to provide the proper environment control for the space station and the 25 kW power module.
Document ID
19780014193
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Maag, C. R.
(Aerojet Electrosystems Co. Azusa, CA, United States)
Millard, J. M.
(Aerojet Electrosystems Co. Azusa, CA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1978
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NASA-CR-150667
REPT-5666-VOL-1
Report Number: NASA-CR-150667
Report Number: REPT-5666-VOL-1
Accession Number
78N22136
Funding Number(s)
CONTRACT_GRANT: NAS8-32637
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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