FIELD: air transport.
SUBSTANCE: hypersonic airplane consists of hull, nose conical part, wings, tail group, fuel tanks, rocket propulsion system and fuel supply pipelines to it. Rocket propulsion system is installed in the rear part of hull and includes turbopump unit with shaft-mounted vanes for oxidiser and fuel, turbine, starting turbine and on-line installed gas generator, two combustion chambers and resonating chambers of combat lasers behind them. Regulator is installed in gas pipeline of one combustion chamber. Combat air craft laser is of electric-discharge type; it is installed at the output of combustion chamber. Inside laser there are electrodes connected to generator installed at turbopump unit of rocket propulsion system.
EFFECT: invention allows improvement of combat characteristics of the airplane.
3 cl, 3 dwg
