FIELD: engine devices and pumps.
SUBSTANCE: method of preparing rocket fuel components for refueling rocket propulsion systems involves the process of thermostating and gas saturation. The process of thermostating and gas saturation is performed in a thermostating and gas saturation unit using a refueling tank truck and auxiliary equipment. The process consists in pumping the fuel components in a closed loop: refueling tanker - thermostating and gas-saturation unit - refueling tanker truck. The refueling tank truck is a mobile unit that provides transportation and temporary storage of fuel components. As an auxiliary equipment, a refrigeration and heating center and a thermal neutralisation unit for the vapour of the fuel components are used.
EFFECT: maintenance of the set parameters of fuel components temperature and gas saturation, increase of mobility and simplicity of operation.
2 dwg, 1 tbl
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