FIELD: cryogenics.
SUBSTANCE: invention can be used as a temperature control system for cryogenic fuel components in the tanks of an encapsulated silo-based rocket. The system includes a launch container 3 installed in the shaft 5 of the silo launcher, which houses a rocket with supporting tanks 1 and 2 with cryogenic fuel. On the inner surface of the launch container there is a heat exchanger, in the lines of which a coolant liquid air circulates, which is supplied into the lines of the container from a Dewar vessel 9. The supply of liquid air in the Dewar vessel 9 is created due to the operation of the air liquefaction unit 7. The Dewar vessel 9 and the air liquefaction unit 7 are located at the head of the launcher 13. The outer surface of the container is covered with a layer of thermal insulation 4.
EFFECT: ensuring long-term storage of cryogenic fuel components in silo-based rocket tanks without refuelling.
2 cl, 1 dwg
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