FIELD: transport; astronautics.
SUBSTANCE: invention is used for launching from Earth both unmanned and manned aerospace vehicle (ASV). Method provides for launching ASV from electromagnetic or gas-dynamic launcher inclined to horizon. At moment of injection of ASV from gun barrel after-threshold intensity laser beam is directed towards it coaxially to gun barrel, beam securing laser-supported detonation wave absorbing laser emission in atmospheric air within limits of said beam. Beam creates plasma channel restructuring shock-wave structure of approach flow near nose part of ASV. Owing to this restructuring aerodynamic drag is decreased during ASV atmospheric penetration. Plasma channel is formed before ASV as long as ASV controls hold it within this channel.
EFFECT: decrease of stalling during aerospace vehicle launching to appointed orbit.
4 dwg
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