AIR THERMOSTATIC CONTROL OF SPACE VEHICLES

FIELD: space engineering. SUBSTANCE: air supply has high-pressure compressed-air receivers communicating through reducer with feed pipeline. The latter communicates with space vehicle through thin- walled pipeline joined by means of on-board connector. Electric heater is made in the form of heat-ins...

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Bibliographische Detailangaben
Hauptverfasser:	KLIMOV V.N, SBORETS V.P, ELISEEV V.G, IGNASHIN A.M, PADZHEV S.M, BARMIN I.V, BAJBAKOV F.B, GOLUBEV B.S, CHECHULIN JU.K, IVANOVA L.P, RAKHMANOV ZH.R, CHUMACHENKO G.F, JUKIN G.L
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBINED HEATING AND REFRIGERATION SYSTEMS HEAT PUMP SYSTEMS HEATING LIGHTING LIQUEFACTION SOLIDIFICATION OF GASES MANUFACTURE OR STORAGE OF ICE MECHANICAL ENGINEERING REFRIGERATION MACHINES, PLANTS OR SYSTEMS REFRIGERATION OR COOLING WEAPONS
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Beschreibung
Zusammenfassung:	FIELD: space engineering. SUBSTANCE: air supply has high-pressure compressed-air receivers communicating through reducer with feed pipeline. The latter communicates with space vehicle through thin- walled pipeline joined by means of on-board connector. Electric heater is made in the form of heat-insulating case filled with liquid antifreeze. Case accommodates coaxially mounted coils connected to feed pipeline; tubular electric heaters of different power are placed in annular gap between coils. The latter are made of stainless steel; ratio of outer diameters of turns of external and internal coils is 1.3-2.0; ratio of total length of coils to inner diameter of coil is between 2000 and 4000. EFFECT: provision for maintaining desired temperature of space vehicle. 2 cl, 3 dwg, 2 tbl