METHOD OF LAUNCHING ROCKET WITH MULTINOZZLE ENGINE

摘要

A method of launching rocket with a multinozzle engine is based on the fact that the start is performed from a starting facility with a slot, through which the gases are passed in the form of a jet from central and side nozzles of the engine and discharged through trays with sidewalls. The sidewalls are mounted outside the surface, which is a boundary area of a supersonic area of engine jets during launch and subsequent departure of the rocket from the launch facility and the flow areas in contact places with the surface of said trays of individual gas-dynamic interacting engine jets are isolated from each other.