首页> 外国专利> Launch complex for small and ultra-small missiles

Launch complex for small and ultra-small missiles

机译:小型和超小型导弹的发射场

摘要

FIELD: aviation.SUBSTANCE: gravity force of accelerating tank with water which through bearing cables and system of units is connected to a launch cage with rocket located therein is used to impart initial acceleration to the rocket. The rocket inside the cage is fixed by pneumatic cylinders symmetrically enclosing the rocket over the entire height. The acceleration of the cage with rocket and accelerating drop of the tank is performed in specially equipped shafts. At the moment of rocket disengagement from the launch cage and activation of cruise engines, discharge valves are opened to empty the accelerating tank. The braking cables connecting the launch cage with brake chains located on the bottom of launch shaft as well as cable brakes are used to stop the system.EFFECT: increase of payload mass delivered by the rocket with the same fuel capacity.6 dwg
机译:领域:航空。物质:加速水箱的重力,水通过轴承电缆和单元系统连接到装有火箭的发射笼上,从而使火箭产生初始加速度。笼子内的火箭由气缸固定,在整个高度上对称地包围着火箭。带有火箭的笼子加速和坦克的加速下落是通过专门配备的轴进行的。在火箭从发射笼中脱离并启动巡航发动机时,打开排放阀以清空加速箱。用于连接发射架和位于发射轴底部的制动链的制动电缆以及电缆制动器用于停止系统。效果:在相同燃料容量的情况下,火箭输送的有效载荷质量增加了6 dwg

著录项

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号