FIELD: rocket; space technology.
SUBSTANCE: invention can be used for ground launch of space rockets and is designed cost-effective launch of payloads into near-Earth orbits. Launch complex for launching a launch vehicle with solid fuel boosters, containing a launch facility, a launch system, a shaft, general technical systems and auxiliary equipment, the launch vehicle has four solid fuel boosters docked to the first stage of the rocket, the booster nozzles are divided into two parts, the lower housings nozzles and upper nozzle housings, in solid fuel boosters there are rods fixed on the launch pad, in which there is a charge of solid fuel with an igniter, high-temperature seals are installed at the ends of the rods, the upper nozzle housings have high-temperature seals and abut against the support grids before the rocket launch, and the ends of the rods abut into the extended support bars, solid fuel charges with igniters are located in the upper bodies of the boosters, when the bars leave the accelerators, the upper and lower bodies form a nozzle, the support bars slide into the upper nozzle body, the bars act as guides during rocket launch.
EFFECT: invention ensures delivery of heavier loads to the near-earth orbit of the Earth.
1 cl, 4 dwg
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Authors
Dates
2023-05-17—Published
2022-12-07—Filed