BTVCS FUNCTIONAL CIRCUIT ON ONE CONTROL CHANNEL OF THE MID-FLIGHT SPACE ROCKET STAGE ENGINE

Abstract

The article is devoted to the development and describing the functional circuit of bifunctional thrust vector control system, consisting of an interceptor unit with fuel component injection, as the executive body of the gas dynamic thrust vector control system for trust vector direction on one regulation channel and exhaust nozzle systems, as the executive body of the additional control system channel.