| 摘要 |
<p>The invention relates to a supersonic airplane, with vertical take-off and landing, used for transportation or military missions. According to the invention, the supersonic airplane is propelled by two orientable turbo-jet engines (2), laterally situated, on some wings (3 and 4) which, during the vertical take-off or landing, may rotate 90 around a transverse axle (6), fastened on the fuselage (1), situated in the airplane centroid area, together with the wings (3 and 4) which flank each turbo-jet engine (2).</p> |
