solid-propellant rocket motor的意思|示意
固体火箭发动机
solid-propellant rocket motor的网络常见释义
固体燃料火箭发动机 solid-propellant rocket motor 固体燃料火箭发动机; 固体推进剂火箭发动机 unguided solid propellant rocket 无控固体推进剂火箭 .
solid-propellant rocket motor相关短语
1、 slow-burning solid-propellant rocket motor 慢燃固体推进剂火箭发动机
2、 Solid propellant ramjet rocket motor 固体火箭冲压发动机
solid-propellant rocket motor相关例句
The effect of radial vibration of the chamber structure composed of propellant grain and case on the internal ballistic property of solid rocket motor (SRM) was investigated.
研究了由推进剂药柱和壳体组成的燃烧室结构径向振动对发动机内弹道性能的影响。
The liner is a polymeric elastomer coating between propellant and insulation layer or case. The liner-forming is a special step in production of solid rocket motor.
衬层是推进剂与绝热层或壳体之间的高分子弹性体涂层，衬层成型是固体火箭发动机生产中的一种特种工序。
The 300mm diameter solid propellant rocket motor employs a composite propellant end burning grain.
直径300毫米的固体推进剂火箭发动机采用了复合推进剂端燃药柱。
A conception of adjustable solid propellant rocket motor was proposed.
本文提出了一种推力可调的固体火箭发动机的设想方案。
Overload acceleration is one of those important factors which influence the performance of solid propellant rocket motor.
过载加速度是影响固体火箭发动机性能的重要因素之一。
Interface bond quality of solid propellant rocket motor can be tested by Lamb waves, but the modes of Lamb waves need to be selected.
用兰姆波可对固体火箭发动机进行胶接质量的检测，但需要对其模式进行选择。