FIELD: transport.
SUBSTANCE: invention relates to rocketry. Gyrating stage comprises nose section and gas generator with pushing, pulling and bank control nozzles. Additionally, said stage comprises sustainer communicated via gas dust and bypass valve with gas generator. Sustainer incorporates thrust vector controls and represents solid propellant engine like gas generator. Gas generator solid propellant charge is made up of cylinder with central bore, its inner and outer surfaces being armored. Gas generator pressure is increased in combustion products overflowing from sustainer. Note here that sustainer and gas generator pressure and charge combustion rate exponents obey definite laws.
EFFECT: higher maneuverability and efficiency.
6 cl, 3 dwg
