Solar concentrator - radiator assembly

A combined solar concentrator and radiator assembly (10) is provided in a relatively lightweight and compact geometry adapted particularly for use in electrical power generation systems in space. The solar concentrator - radiator assembly comprises a solar reflector of the Cassegrain type having pri...

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Bibliographische Detailangaben
Hauptverfasser:	MORIARTY, MICHAEL P
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION BLASTING COSMONAUTICS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS 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 MECHANICAL ENGINEERING PERFORMING OPERATIONS RANGES REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGYGENERATION, TRANSMISSION OR DISTRIBUTION SOLAR HEAT COLLECTORS SOLAR HEAT SYSTEMS TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR VENTILATING WEAPONS
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Beschreibung
Zusammenfassung:	A combined solar concentrator and radiator assembly (10) is provided in a relatively lightweight and compact geometry adapted particularly for use in electrical power generation systems in space. The solar concentrator - radiator assembly comprises a solar reflector of the Cassegrain type having primary and secondary reflelctor surfaces (14) and (26) for concentrating incident solar ration upon a thermal powered generator unit (16). The primary reflector surface (14) is formed on one side of an array of interleaved panels (30) adapted for movement between a compact stowed profile to fit within the cargo bay of a transport vehicle, and an extended deployed configuration. The reverse sides of these panels define a space radiator of extended surface area connected to the generator unit (16) by heat transfer members such as heat pipes (34) for purposes of dissipating excess heat to the surrounding space environment.