FIELD: launching devices.
SUBSTANCE: invention relates primarily to ground-based means of launching space rockets. The launch complex is equipped with accelerator-refueling side blocks (ARB) connected to the rocket with stationary rods installed inside them - separately for oxidizer and fuel. In the rods, as well as between the ARB and the rods, cavities are formed, where high-pressure fuel components are supplied using a pump-compressor system, which are then fed into the regular rocket tanks, from which its engines are powered. Thus, when rising to a height of 40-60 m, the rocket tanks remain full, and then the ARB, having consumed fuel from the above cavities, are separated. Due to the high pressure in the cavities, when the rocket is lifted, an additional lifting force acts on it.
EFFECT: increase in the mass of the payload put into orbit around the Earth, as well as the safety of a rocket launch in a strong side wind.
1 cl, 8 dwg
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Authors
Dates
2023-01-24—Published
2022-11-23—Filed