Locking device for air-to-air guided missiles

摘要

An air-to-air guided missile with solid propellant rocket motor is retained by a locking device having a blocking device during a predeterminable delay time after the rocket motor has been fired. Thereby, at high altitude or with a high speed, such a proportion of the propellant can be burnt off that the guided missile is not accelerated to an inadmissibly high speed.