RADIATOR FOR ARTIFICIAL SATELLITE

RADIATOR FOR ARTIFICIAL SATELLITE

PROBLEM TO BE SOLVED: To provide a radiator for an artificial satellite to bring the interior of the artificial satellite into a proper temperature (-40°C to +60°C) even when it is receiving sunlight about 10 times as strong and planet radiation 20 times as strong as those receiving when it is in or...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: DOWNAR HARTMUT, FAUST THOMAS
Format: Patent
Sprache:eng
Schlagworte:
AIRCRAFT
AVIATION
BLASTING
COSMONAUTICS
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
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
WEAPONS
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Beschreibung
Zusammenfassung:PROBLEM TO BE SOLVED: To provide a radiator for an artificial satellite to bring the interior of the artificial satellite into a proper temperature (-40°C to +60°C) even when it is receiving sunlight about 10 times as strong and planet radiation 20 times as strong as those receiving when it is in orbit near the earth. SOLUTION: In the radiator for the artificial satellite SAT, a wavelength selecting element has total high semi-sphere emissive profile and low absorption index profile of as opposed to infrared radiation of compatible black body for a certain temperatures from 500K to 700K, and low sunlight absorption index profile. COPYRIGHT: (C)2004,JPO