| 摘要 |
FIELD: aviation and space engineering. SUBSTANCE: flying vehicle has thermal jet propeller 1 made in form of saucer on whose bottom helicopter rotor 2 is mounted forming monoblock. For rectilinear motion of vehicle in space, fire-type jet engine 6 is mounted with telescopic nozzle. For change of direction of motion of flying vehicle, fire-type attitude-control jet engines 7 and brake engines 8 are mounted. Cabin 5 may be mounted above or below propeller 1 for reversible motion relative to saucer in horizontal plane. Efficiency of propeller ranges from 0.9 to 0.95. No special training of astronauts and passengers is required. G-loads at vertical take-off and flight at speed of 25 to 35 m/s are absent due to availability of rotary thermal field in front of flying vehicle. EFFECT: ecological safety, noiseless flight and low cost. |
