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- liquid rocket thruster 液体火箭发动机
- The leak of Liquid Rocket Engine (LRE) is very common and dangerous. 液体火箭发动机的泄漏是常见和极其危险的故障。
- Valler HW. Performance of a Transpiration-regenerative Cooled Rocket Thrust Chamber. NASA CR159742, N80-14189. 宁建华.;光刻技术在液体火箭发动机的应用
- The rocket thrusted away from Earth. 火箭从地球上猛冲出去。
- If the object needs to be sufficient to leave the Earth's energy rocket thrust, to generate enough speed in order to leave Earth's gravity and the atmosphere over. 如果要使物体离开地球必须需要足够能量的火箭推力，来产生足够的速度，这样才能离开地球的引力而飞越过大气层的。
- The integrity test of Liquid Rocket Engine (LRE) must be carried out before its launch. 在液体火箭发动机发射前，必须进行完整性试验。
- Vacuum vessel seal structure used in the leak test of a liquid rocket engine turbopump is discussed. 论述了某型号液体火箭发动机涡轮泵高压低温静密封检漏试验用真空室密封结构的设计问题。
- The study may be helpful for fault diagnostics of the start up of liquid rocket engine (LRE). 为液体火箭发动机启动过程的故障诊断提供参考依据。
- Rotor dynamic is one of the most complicated problems in development of LOX turbopump of liquid rocket engine. 转子动力学问题是液体火箭发动机研制中最复杂的问题之一。
- Unsymmetrical dimethylhydrazine (UDMH) is the main fuel of liquid rocket propellant. Stress is always laid on the pollution of UDMH to water. 偏二甲肼(UDMH)是液体推进剂的主体燃料,其对水体的污染一直倍受重视。
- Spin often interferes with internal operation of liquid rockets. 液体火箭的旋转常常会干扰其内部工作。
- Abstract: To review the progress in the major ass ignment, the organization and implementation of protection against liquid rocket propellent. 文摘:综述了发射大型运载火箭推进剂作业卫勤保障主要任务、保障重点、卫勤力量的分配、卫勤保障的组织和实施进展。
- Abstract ：To review the progress in the major ass ignment, the organization and implementation of protection against liquid rocket propellent. 摘要 ：综述了发射大型运载火箭推进剂作业卫勤保障主要任务、保障重点、卫勤力量的分配、卫勤保障的组织和实施进展。
- To review the progress in the major ass ignment, the organization and implementation of protection against liquid rocket propellent. 综述了发射大型运载火箭推进剂作业卫勤保障主要任务、保障重点、卫勤力量的分配、卫勤保障的组织和实施进展。
- Sound Field Analysis on Thrust Chamber of Liquid Rocket 液体火箭发动机推力室内声场分析
- Technology of loxodrome coolant channel machining on liquid rocket engine. YUHANG XUEBAO/Journal of Astronautics. Vol.24 No.3. May,2003. Wang Yongqing, Lu Jiechi,Tong Yu. 等倾角螺旋槽的片铣刀铣削加工技术.;工具技术
- This paper mainly discusses available structures of the liquid hybrid bearings and the key technologies that need to be solved for the liquid rocket engine turbopump. 针对液体火箭发动机涡轮泵特殊工作环境,讨论了流体动静压轴承可采用的结构形式和需要解决的关键技术。
- By analyzing the working characteristics of the liquid rocket engine, strategies of applying data mining from the point of view of the data warehouse for FDD of LRE are proposed. 分析表明,聚类、类、联、间序列分析和孤立点检测等数据挖掘方法适用于液体火箭发动机的故障检测和诊断。
- Coaxial hydrogen/oxygen resonance ignitor is non-electric and bluntly sensible, which is good ignition scheme for the developing reusable liquid rocket engine. 非电钝感的同轴氢氧谐振点火器可作为正在研究发展中的可重复使用液体火箭发动机多次点火的优选方案之一。
- Calibration on rocket thrust vector measuring system 对火箭发动机推力矢量测试系统的标定
