FIELD: fuel systems of flying vehicles, mainly special heavy aeroplanes including external tanks. SUBSTANCE: fuel tank includes shell and fuel suction device. Shell has front and rear end shields and inner cavity filled with fuel. Granulated hydrocarbon polymer material is used as fuel. Inner cavity of tank is provided with axially movable piston. Fuel suction device is located between working surface of piston and rear end shield. EFFECT: improved explosion-proof and fire safety properties; extended range of application. 17 cl, 5 dwg
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