Launch vehicle (HER OPTIONS) AND METHOD OF ITS CRACKDOWN ON ITS PATH active sites

摘要

1. The launcher, including the multi-stage, each stage of which comprises a liquid-propellant rocket motors, tanks for propellant components and a payload, which in the general case are either following stage with its payload, or directly to the payload, wherein that the bins for different propellant components each or at least the first stage are made structurally isolated as separate units and are disposed parallel to each other parallel to the longitudinal axis of the missile-n CITEL, forming a plurality of parallel arranged blokov.2. The launcher, including the multi-stage, each stage of which comprises a liquid-propellant rocket motors, tanks for components propellant and a payload, which in the general case are either following its steps with the payload, or directly to the payload, characterized in that bins for different propellant components each or at least the first stage are made coaxial, and one of the tanks for one of the propellant components situated inside the tank for a second component of rocket fuel, and wherein the lower and upper parts, at least one tank, respectively, are attached to block liquid rocket engines and the payload, and the inner tank walls are also internal and external walls baka.3. The launcher, including the multi-stage, each stage of which comprises a liquid-propellant rocket motors, tanks for propellants and a payload, which in the general case are either following stage with its