Multi-directional cooler

Heat exchange – Movable heating or cooling surface – Rotary drum

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Details

165 41, 165904, 244163, F28D 1502, B64G 150

Patent

active

053320301

ABSTRACT:
A passive thermal control system for use in a spacecraft or satellite. The system uses at least two heat pipe and radiator systems connected to a heat generating load of the spacecraft. The radiators are located at different sides of the spacecraft. The heat pipes can be prevented from transferring heat from the radiators to the heat generating load such that a first radiator can be exposed to heat from sunlight while the second radiator and heat pipe can still operate to remove heat from the heat generating load.

REFERENCES:
patent: 3402761 (1968-09-01), Swet
patent: 3489203 (1970-01-01), Fischell
patent: 3749156 (1973-07-01), Eby et al.
patent: 4133376 (1979-01-01), Eilenberg et al.
patent: 4162701 (1979-07-01), Ollendorf
patent: 4388964 (1983-06-01), Almgren et al.
patent: 4420035 (1983-12-01), Hewitt
patent: 4673030 (1987-06-01), Basiulis
patent: 4757688 (1988-07-01), Basiulis et al.
patent: 4880050 (1989-11-01), Nabamura et al.
"A Variable-Conductance Heat Pipe Radiator for Marots-Type Communications Spacecraft" by Savage et al., Journal of Spacecraft, May-Jun. 1979, vol. 16, No. 3, pp. 176-180.

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