A plurality of two adjacent heat pipes in a single layer for equipment radiator panels

Heat dissipating apparatus for use on a spacecraft having heat generating elements 11 disposed on panels 22. The heat dissipating apparatus comprises a plurality of two adjacent heat pipes disposed in a single layer 13. The said heat pipes 13 may be selectively disposed on non radiating surfaces of...

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Bibliographische Detailangaben
Hauptverfasser:	ALAN L SPENCER, JASON J CHIANG
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION BLASTING CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS COSMONAUTICS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY HEAT EXCHANGE IN GENERAL HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT HEATING LIGHTING MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS MECHANICAL ENGINEERING PERFORMING OPERATIONS PRINTED CIRCUITS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS
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Beschreibung
Zusammenfassung:	Heat dissipating apparatus for use on a spacecraft having heat generating elements 11 disposed on panels 22. The heat dissipating apparatus comprises a plurality of two adjacent heat pipes disposed in a single layer 13. The said heat pipes 13 may be selectively disposed on non radiating surfaces of the panels 22, or between the outer and the inner surfaces 22a, 22b of the panels 22. Heat generating elements 11 are disposed opposite to the said heat pipes 13. Preferably, the heat generating elements 11 are components such as travelling wave tube, channel, power amplifiers, and the arrangement of the said heat pipes 13 comprise a plurality of 'U' shaped heat pipes 13 nestled/interlinked with adjacent 'U, shaped heat pipes 13.