Passive thermal radiator for earth orbiting satellite

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

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244163, 165 6, B64G 146, B64G 154

Patent

active

046696857

ABSTRACT:
An earth orbiting satellite (10) having an interior portion (22) supporting heat generating elements (26) and an exterior portion (12) having a thermal radiator (20) for heat radiated by these elements, is provided with reflectors (34s, 34c) in the annulus between the interior and exterior portions, the reflectors being configured to reflect radiation from the axially extending side surfaces of the heat generating elements to the thermal radiator and to conduct heat from the heat generating elements and radiate the conducted heat to the thermal radiator.

REFERENCES:
patent: 2234122 (1941-03-01), Heck
patent: 3310102 (1967-03-01), Trombe
patent: 3596853 (1971-08-01), Anderson
patent: 3768754 (1973-10-01), Janes
patent: 4423605 (1984-01-01), Petrick et al.

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