| 摘要 |
FIELD: space.SUBSTANCE: invention relates to space engineering and can be used in flight in open space, and in atmosphere. Aircraft comprises two rigidly connected to each other jet engines, housing and cylinder. In cylinder there is a piston with jet engine. Exhaust pipes and shock absorber are rigidly connected with cylinder. Shock absorber provides movement of housing in forward direction, and piston in reverse direction. Shock absorber is hydraulically connected with control unit of shock absorber. Downward-bent exhaust pipe is rigidly connected to housing is placed in front of nozzle and after bending come out of housing behind it. Air intake device is arranged at joint of front part of housing. Shock absorber control unit is configured to mix air jet with an oxidising agent and has hydraulic inlet connected with hydraulic outlet of air intake device.EFFECT: technical result is increase of aircraft velocity in atmosphere without increasing number of fuel components.1 cl, 1 dwg |
