Title:
RADIATOR FOR ARTIFICIAL SATELLITE
Document Type and Number:
Japanese Patent JP2004001739
Kind Code:
A
Abstract:
To provide a radiator for an artificial satellite to bring the interior of the artificial satellite into a proper temperature (-40°C to +60°C) even when it is receiving sunlight about 10 times as strong and planet radiation 20 times as strong as those receiving when it is in orbit near the earth.
In the radiator for the artificial satellite SAT, a wavelength selecting element has total high semi-sphere emissive profile and low absorption index profile of as opposed to infrared radiation of compatible black body for a certain temperatures from 500K to 700K, and low sunlight absorption index profile.
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Inventors:
FAUST THOMAS
DOWNAR HARTMUT
DOWNAR HARTMUT
Application Number:
JP2003137913A
Publication Date:
January 08, 2004
Filing Date:
May 15, 2003
Export Citation:
Assignee:
ASTRIUM GMBH
International Classes:
B64G1/50; F28D21/00; (IPC1-7): B64G1/50; F28D21/00
Attorney, Agent or Firm:
Takashi Watanabe
Masatake Shiga
Tadashi Takahashi
Masakazu Aoyama
Suzuki Mitsuyoshi
Kazuya Nishi
Yasuhiko Murayama
Shinya Mitsuhiro
Masatake Shiga
Tadashi Takahashi
Masakazu Aoyama
Suzuki Mitsuyoshi
Kazuya Nishi
Yasuhiko Murayama
Shinya Mitsuhiro
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