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Space Station Freedom photovoltaic power module design statusElectric power generation for Space Station Freedom will be provided by four photovoltaic (PV) power modules using silicon solar cells during Phase 1 operation. Each PV power module requires two solar arrays with 32,800 solar cells generating 18.75 kW of dc power for a total of 75 kW. A portion of this power will be stored in nickel-hydrogen batteries for use during eclipse, and the balance will be processed and converted to 20 kHz ac power for distribution to end users through the power management and distribution system. The design incorporates an optimized thermal control system, pointing and tracking provision with the application of gimbals, and the use of orbital replacement units (ORU's) to achieve modularization. Design status of the PV power module, as derived from major trade studies, is discussed at hardware levels ranging from component to system. Details of the design are presented where appropriate.
Document ID
19890015902
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jimenez, Amador P.
(Rockwell International Corp. Canoga Park, CA., United States)
Hoberecht, Mark A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1989
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-102073
NAS 1.15:102073
E-4832
Meeting Information
Meeting: Intersociety Energy Conversion Engineering Conference
Location: Washington, DC
Country: United States
Start Date: August 6, 1989
End Date: August 11, 1989
Sponsors: SAE, AIChE, ASME, IEEE, ACS, ANS, AIAA
Accession Number
89N25273
Funding Number(s)
PROJECT: RTOP 474-46-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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