FIELD: aircraft engineering.
SUBSTANCE: aircraft consists of airframe and engine with exhaust nozzle. Airframe comprises parachute compartment and parachute ejector wit input connected with appropriate control unit and with moving plate coupled with the drive, its input being connected with the drive control unit output. Parachute compartment is arranged at mid top section, above moving plate and below parachute ejection control unit. Pulse engine with exhaust nozzle is additionally arranged under airframe front. Rotary sector spring-loaded shutter is arranged ahead of said nozzle. Vertical prop is arranged behind said shutter coupled therewith after the turn.
EFFECT: efficient deceleration.
1 dwg
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Authors
Dates
2015-04-10—Published
2014-03-13—Filed