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Title:
SOLAR GENERATOR FOR SPACECRAFT
Document Type and Number:
Japanese Patent JPS60142554
Kind Code:
A
Abstract:

PURPOSE: To reduce the thermal stress upon a framework and a panel sheet after a solar generator is extended in the space by a method wherein a panel sheet is provided with stress only when it is retracted utilizing an auxiliary bar fixed on the panel sheet.

CONSTITUTION: An auxiliary bar 9 fixed on a proper position using an adhesive on a panel sheet 1 fitted with solar battery cells 4 is formed higher than horizontal beams 2a. When this solar generator is retracted by hinges 3 to push a panel sheet 1 adjoining the auxiliary bar 9 out of the surface, the flexible panel sheet 1 is deformed to provide itself with tension preventing the panel sheet 1 from vibrating under any vibration load. After the solar generator is extended in the space, the panel sheet 1 may be deprived of the tension to reduce the thermal stress due to solar heat.


Inventors:
TSUKUI KEITAROU
INOUE AKIO
YAMAMOTO KAZUO
Application Number:
JP24572583A
Publication Date:
July 27, 1985
Filing Date:
December 29, 1983
Export Citation:
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Assignee:
MITSUBISHI ELECTRIC CORP
International Classes:
H01L31/042; B64G1/22; B64G1/44; (IPC1-7): H01L25/04; H01L31/04
Attorney, Agent or Firm:
Masuo Oiwa



 
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