FIELD: weapons and ammunition.
SUBSTANCE: in compliance with first version, rocket comprises liquid-propellant engine, tanks and pulsating generator. The latter is composed of closed chamber operating on rocket fuel components. Its inlets are communicated with fuel tanks fluid sections via check valves and its outlets are communicated with fuel tank gas sections. Gas generator or tanks are equipped with safety valves. In compliance with another version, fuel components are fed in gas generator by two articulated displacement pumps. In compliance with the other version, rocket comprises gas generator charge communicated via check valves with tank gas sections. In compliance with one more version, fuel tanks are provided with separation bellow or elastic bag secured to tank outlet or opposite it. In other version, every fuel tank has separation web with bypass acceleration valve opening in direction opposite the thrust vector. In one more version, rocket incorporates two vibratory or rotary displacement pumps to feed fuel in oxidiser tank and oxidiser into fuel tank, respectively.
EFFECT: decreased weight and dimensions.
20 cl
