| 摘要 |
The invention relates to the aerospace industry, and specifically to aerospace aircraft performing flights in the atmosphere of planets at hypersonic velocities. This invention makes it possible to perform flights in the atmosphere of planets at velocities of greater than Mach 50, which significantly exceeds the possibilities of already known devices. What is known is: a method for moving in an atmosphere of planets at cosmic velocities exceeding the local orbital velocity at which the aircraft performs braking with the aerodynamic plane at velocities greater than the first cosmic velocity and even the third cosmic velocity. However, such methods are directed only to braking spacecraft when returning from space expeditions. This method does not make possible to perform a cruise flight in the atmosphere starting from the surface of a planet and is also not capable of accelerating in the upper layers of the atmosphere to velocities exceeding the first cosmic velocity without moving out into outer space since the centrifugal force of the local orbital cosmic velocity exceeds the force of gravitation. Also known are devices comprising hypersonic aircraft performing a flight in the upper layers of the atmosphere which are not capable of achieving the first cosmic velocity whilst performing further acceleration as a result of the incapacity for full combustion of fuel in hypersonic direct-flow chambers and a weak system of air inlets as well as the extremely high temperature conditions to which the air frame and the elements thereof (pillars, empennage, air inlets, projecting portions, pods etc.) of hypersonic aircraft are subjected. |
