DEVICE FOR THERMOSTATING OF SPACE OBJECTS

FIELD: rocket-space engineering equipment. SUBSTANCE: device comprises pressurized air source in the form of compressor-charged receivers, feeding pipeline with filter and regulating fittings, on-board detachable connection means, thin- walled pipeline arranged along rocket vertical axis, cooler for...

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Bibliographische Detailangaben
Hauptverfasser:	SBORETS V.P, RAKHMANOV ZH.R, CHUMACHENKO G.F
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: rocket-space engineering equipment. SUBSTANCE: device comprises pressurized air source in the form of compressor-charged receivers, feeding pipeline with filter and regulating fittings, on-board detachable connection means, thin- walled pipeline arranged along rocket vertical axis, cooler for air and liquid pipelines connected with cooler and having locking-and-regulating fittings. Device has vessel with cooling liquid, pump and cooling means, electrical heater and control panels. Cooler for air disposed after electrical heater is made in form of heat-insulated metal body and has gate, safety valve, drainage valve and supports. Feeding pipeline is connected to inlet and outlet ends of coaxial coils. Coaxial coils are formed by two-layer winding of pipes on hollow sealed cylinder alternately with padding. Ratio of cylinder length l to outer diameter Dout is in the range of 1,2