DocumentCode
2544972
Title
Launch packaging options for the PV power module cargo element
Author
Hoberecht, Mark A. ; Vogt, Scott T.
Author_Institution
NASA Lewis Res. Center, Cleveland, OH, USA
fYear
1989
fDate
6-11 Aug 1989
Firstpage
295
Abstract
The development of photovoltaic (PV) power module cargo element for the Space Station Freedom is discussed. The PV power module consists of several unique assemblies, each with its own function. These assemblies are combined in such a manner that functions are consolidated and packaging is efficient. Several packaging options for the PV power module cargo element are presented. These options are discussed in terms of their impact on the overall flight hardware manifest as determined by the various constraints. Space Station Freedom program considerations are also addressed
Keywords
solar cell arrays; space vehicle power plants; PV power module; Space Station Freedom; assemblies; development; flight hardware manifest; packaging; solar cell arrays; space power; Assembly; Electronic packaging thermal management; Hardware; Multichip modules; NASA; Packaging machines; Space shuttles; Space stations; Thermal management of electronics; Transportation;
fLanguage
English
Publisher
ieee
Conference_Titel
Energy Conversion Engineering Conference, 1989. IECEC-89., Proceedings of the 24th Intersociety
Conference_Location
Washington, DC
Type
conf
DOI
10.1109/IECEC.1989.74478
Filename
74478
Link To Document