FIELD: transportation.
SUBSTANCE: airplane comprises fuselage, front and back wings, gas-turbine engines installed on wings, and rocket engine installed in back part of fuselage. On upper part of fuselage along its longitudinal axis there is aviation-based fighting laser installed, which is connected by air sampling pipelines that comprises controller valve to at least one gas-turbine engine and with rocket engine. Laser is arranged as gas-dynamic, comprises optical head and exhaust system, is connected by air sampling pipeline comprising controller valve to turbo-pump set downstream turbine.
EFFECT: improved fighting properties of airplane.
5 cl, 5 dwg
