Earth orbiting satellite with improved passive thermal radiator

Aeronautics and astronautics – Spacecraft – Spacecraft formation – orbit – or interplanetary path

Patent

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Details

244158A, 244163, 165903, B64G 150

Patent

active

045807485

ABSTRACT:
An earth orbiting satellite (10) having a despun interior portion (22) supporting heat generating elements (24) and a spinning exterior portion (12) having a thermal radiator (20) for heat radiated by these elements, is provided with reflectors (42, 44) in the annulus (40) between the spinning and despun portions, the reflectors being configured to reflect radiation from the annulus to the thermal radiator. See FIG. 2.

REFERENCES:
patent: 2234122 (1941-03-01), Heck
patent: 3310102 (1967-03-01), Trombe
patent: 3422886 (1969-01-01), Baller
patent: 3489203 (1970-01-01), Fischell
patent: 4162701 (1979-07-01), Ollendorf
patent: 4423605 (1984-01-01), Petrick et al.

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