| 摘要 |
The present invention relates to a method for damping the acoustic pressure during firing of missiles (2), which are rocket-propelled or ramjet-propelled in their trajectory, when these are launched from their missile tube (1) by a starter motor (3) of the gas generator type which is secured in the missile tube (1). According to the invention, the acoustic pressure is damped by the effect which arises when propellant gases from the starter motor (3) shatter one or more liquid-filled containers (4) arranged in the gas exhaust opening of the missile tube. |
