FIELD: flying vehicles.
SUBSTANCE: proposed aircraft has fuselage, pilot's cabin in nose section and turbo-jet engines. Fuselage has rounded-off top and hull-type bottom with landing units on shock-absorber struts and hatches. Turbo-jet engines are provided with controllable nozzle for change of angle of inclination of gas jet; they are mounted on pylons on sides of fuselage; pylons are mounted above longitudinal axis of fuselage and on surface of its tail section. Piloting and maneuvering of aircraft are performed through change of angle of inclination of nozzle of turbo-jet engines and their thrust. Fuselage may be provided with passenger saloon and cargo compartment. Tail section of flying vehicle fuselage is provided with hatches and mechanisms for pan-caking of detachable fuel tanks or cargoes under adverse conditions of flight.
EFFECT: simplified arrangement.
3 cl, 2 dwg
| Title | Year | Author | Number |
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