LPRE：液体火箭发动机
液体火箭发动机（Liquid Propellant Rocket Engine，简称LPRE）是一种广泛应用于航天及军事领域的高性能推进系统，其缩写形式LPRE便于书写与交流，常见于专业文献及技术文档中。
Liquid Propellant Rocket Engine具体释义
Liquid Propellant Rocket Engine的英文发音
例句
- Based on the requirements for development of liquid propellant rocket engine and shaped charge warhead, the manufacturing technique of their key parts was researched.
- 结合液体火箭发动机(LPRE)和破甲弹的发展需求，将磨擦辅助精密电铸技术应用于其关键零件的制造。
- Concrete steps and some effective measures for improving the liquid propellant rocket engine which is weak in the tangential mode of high frequency stability are also described in the paper.
- 根据所得结果，为此发动机中安装径向隔板的必要性提供了理论依据井对稳定性不佳的液体火箭发动机(LPRE)提出了具体改进步骤及一些有效措施。
- A calculation of the wall temperature distribution in liquid propellant rocket engine chamber with milled grooves was completed by the aid of three-dimensional finite element method.
- 采用三维有限元模型对液体火箭发动机(LPRE)铣槽推力室进行了壁温分布计算。边界条件按一维经验公式处理。
- Particle Swarm Optimization Algorithm Based Damage-mitigating Control for Reusable Liquid Propellant Rocket Engine(LPRE)
- 基于粒子群算法的可重复使用液体火箭发动机(LPRE)减损优化问题研究
- To verify the effectiveness of the control method, the digital simulation of controlling the variable thrust liquid propellant rocket engine with this controller is presented.
- 变推力液体火箭发动机(LPRE)可以满足这一要求，但当发动机的推力大范围变化时，发动机的动态特性随之变化，这使得简单的反馈控制难以满足控制要求。
本站英语缩略词为个人收集整理，可供非商业用途的复制、使用及分享，但严禁任何形式的采集或批量盗用
若LPRE词条信息存在错误、不当之处或涉及侵权，请及时联系我们处理：675289112@qq.com。