FIELD: rocketry; multi-stage liquid-propellant rockets. SUBSTANCE: multi-stage rocket comprises tandem stage with separation devices, rocket engines and tanks for liquid propellant components. Tank of previous stage of one propellant component is divided into front and rear sections by tank of other component; engine of subsequent stage is sunk in first section; provision is made for devices for communication with surrounding medium. EFFECT: reduction of power requirements for control of flight and structural mass. 2 cl, 1 dwg
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Authors
Dates
1997-08-10—Published
1994-09-27—Filed