FIELD: aeronautical engineering. SUBSTANCE: pressure in filling reservoir 5 is maintained at minimum permissible level below working pressure in tank 1 being filled: transfer of propellant to tank 1 is effected with the aid of transfer pump 9 mounted in filling reservoir above zone of solidification of gas admixtures. EFFECT: filling the flying vehicle with purified cryogenic propellant and reduction of solidified harmful impurities in flying vehicle tanks. 1 dwg
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