FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed drone plane features normal aerodynamic configuration and comprises fuselage, high-set three-spar wing, two-fin vertical unit and all-moving tailplane with differential control. Rear edge of every outer wing accommodates flaps, ailerons and stall fence. Landing gear is a tricycle landing gear type. Main legs are retracted into fuselage and incorporate one large-diametre wheel. Nuclear engine represents power plant made up of low-temperature nuclear synthesis reactor incorporating neutron generator with lithium-7 isotope, a reagent, to generate steam for turbine coupled with compressor wherein air is compressed and heated for nozzle to generate thrust.
EFFECT: expanded operating performances.
7 dwg
