Direct condensation radiator for spacecraft

Details Direct condensation radiator for spacecraft Direct condensation radiator for spacecraft

1986-03-12

1988-04-19

Davis, Jr., Albert W.

Heat exchange

With alarm, indicator, signal, register, recorder, test or...

Remotely controlled inspection means

165 111, 165 41, 165 70, 244158R, 244163, F28F 1100, F28F 2702, B64G 156, B64G 144

Patent

active

047383046

ABSTRACT:
Cost and weight of a heat transfer structure for a space vehicle can be reduced by an arrangement of redundant channels for the flow of coolant to heat radiating panels, micrometeroid resisting bumpers located adjacent the channels for preventing penetration by all but the most energetic micrometeroids, and a sensing and control arrangement for sensing the penetration of a coolant channel for shutting off that channel to prevent loss of coolant.

REFERENCES:
patent: 3211215 (1965-10-01), Walker
patent: 3239164 (1966-03-01), Rapp
patent: 3435889 (1969-04-01), Bienert
patent: 3517730 (1970-06-01), Wyatt
patent: 3532158 (1970-10-01), Hiebert
patent: 4161212 (1979-07-01), Hightower
patent: 4516631 (1985-05-01), Russell

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