前言飞机外挂物弹射式发射产生的动力响应严重危及外挂设备和结构的可靠性。例如,当“白星眼”滑翔炸弹用高压火药柱弹射发射时,有制导随时间变化的问题。因此,对用于弹射发射“白星眼”导弹的火药柱实行限制。同样,对其它一些弹射式发射外挂物也实行限制。因此,包括“捕鲸叉”导弹在内的现行机上发射武器的研制计划都对弹射冲击环境非常关注。过去,完成了各种试验计划,以测定飞机外挂物弹射式发射的冲击环境。然而,大多数 INTRODUCTION The dynamic response resulting from the ejection of aircraft plug-ins seriously jeopardizes the reliability of plug-in equipment and structures. For example, when the “White Star Eye” glide bomb was fired with a high-pressure powder column, there was a problem with guidance over time. Therefore, a limit was imposed on the powder pellets used for the catapult launch of the “White Star Eye” missile. Similarly, there are restrictions on some other catapult launchers. Therefore, the current plan of launching weapons on board, including “whaling” missiles, is of great concern for the impact environment. In the past, various pilot programs have been completed to determine the impact environment of the aircraft plug-in projectile launch. However, most