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The Solar Dynamic radiator with a historical perspectiveA historical perspective on pumped loop space radiators provides a basis for the design of the Space Station Solar Dynamic (SD) power module radiator. SD power modules, capable of generating 25 kWe each, are planned for growth Station power requirements. The Brayton (cycle) SD module configuration incorporates a pumped loop radiator that must reject up to 99 kW. The thermal/hydraulic design conditions in combination with required radiator orientation and packaging envelope form a unique set of constraints as compared to previous pumped loop radiator systems. Nevertheless, past program successes have demonstrated a technology base which can be applied to the SD radiator development program to ensure a low risk, low cost system.
Document ID
19890027969
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mclallin, K. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Fleming, M. L.
(LTV Corp. Missiles and Electronics Group, Dallas, TX, United States)
Hoehn, F. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Howerton, R.
(Rockwell International Corp. Rocketdyne Div., Canoga Park, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 1988 IECEC
Location: Denver, CO
Country: United States
Start Date: July 31, 1988
End Date: August 5, 1988
Accession Number
89A15340
Distribution Limits
Public
Copyright
Other

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