A Contact Conductance Interface for a Space Constructable Heat Pipe Radiator
A Contact Conductance Interface for a Space Constructable Heat Pipe Radiator
- Neue Suche nach: Oren, John A.
- Neue Suche nach: Fleming, Michael L.
- Neue Suche nach: Oren, John A.
- Neue Suche nach: Fleming, Michael L.
A connectable/disconectable thermal interface has been developed for the constructable radiator system under development at NASA-Johnson Space Center. A contact heat exchanger approach which involves pressurized clamping of a segmented cylindrical heat exchanger on the outside of a round heat pipe evaporator section was designed, fabricated, and tested. Dry metal-to-metal contact conductance heat transfer is utilized. Test results have indicated excellent contact conductances of up to 8500 w/m2°c (1500 Btu/ft2°F) at 2000 kPa (300 psi) clamping force. The feasibility and fabricability of the design have been demonstrated.
Dokumentinformationen
A Contact Conductance Interface for a Space Constructable Heat Pipe Radiator
Sae Technical Papers
Intersociety Conference on Environmental Systems ; 1983
1983-07-11
Aufsatz (Konferenz)
Englisch
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