FLYING MACHINE, ESPECIALLY MISSILE OR ROCKET, COMPRISING TWO SEPARABLE PARTS ON A PATH

摘要

P The present invention relates to a flying machine, in particular a missile, comprising two parts (20, 30), respectively a front part (20) and a rear part (30) intended to be separated on the trajectory, characterized in that it further comprises an asymmetrical wing (50) linked to the rear part (30) and making it possible to ensure a divergence between the paths of the two parts. /P