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- Another unconventional design element, the hybrid rocket engine that powers the suborbital vehicle, provides unique operational options. 另一个异于传统的设计要素，是提供次轨道载具动力的混合式火箭引擎，它能提供独特的操作选择。
- Grain design for hybrid rocket engine with cluster type thrust chamber 带簇式推力室的固液火箭发动机装药设计
- hybrid rocket engine 固液混合发动机
- Altman D. Hybrid rocket development history. AIAA Paper 91-2515. 单建胜等.;固液火箭发动机的研制及其应用
- 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。
- For one thing, they simplify the design of a rocket engine. 首先，它们可以简化火箭发动机的设计。
- The rocket engine carries with it the oxygen of its own . 火箭发动机自带氧气。
- Mo nozzle for the rocket engine nozzle professional. 钼喷嘴专业用于火箭发动机喷嘴。
- Armstrong and Aldrin fired the lander rocket engine. 阿姆斯特朗和奥尔德林点燃了登月舱的火箭发动机。
- Estey Paul N, Whittinghill Geroge R. Hybrid rocket motors propellant selection alternative. AIAA Paper 92-3592. 单建胜等.;固液火箭发动机的研制及其应用
- Kniffen B J. Hybrid rocket development at the American rocket company. AIAA Paper 90-2762. 单建胜等.;固液火箭发动机的研制及其应用
- Unlike a rocket engine, the jet engine, as you konw, is an "air breather" . 正如你们所知道的，这种喷气发动机与火箭发动机不同：它是“空气喷气发动机。”
- Chiaverini, M.J. et.Al., “Pyrolisis Behavior of Hybrid Rocket Solid Fuels Under Rapid Heating Conditions,” AIAA Paper No. 97-3078, 1997. 施耿维;“混合推进剂燃烧组织与性能”;国立成功大学航空太空工程研究所硕士论文(1999).
- Unlike a rocket engine, the jet engine, as you know, is an "air breather". 正如你们所知道的，这种喷气发动机与火箭发动机不同：它是“空气喷气发动机”。
- Chiaverini, M.J. et.Al., ”Fuel Decomposition and Boundary Layer Combustion Processes of Hybrid Rocket Motors,” AIAA Paper 95-2686, 1995. 林涌丰;“混合火箭燃烧特性之研究”;国立成功大学航空太空工程研究所硕士论文(2000).
- 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。
- Numerical solutions of full Navier-Stokes equations with chemical reaction flow were obtained for of the LOX/HTPB hybrid rocket motor. 利用二维轴对称N-S方程和组分方程对选用液氧/端羟基聚丁二烯推进剂的固液混合火箭发动机的燃烧室和喷管进行了一体化计算。
- It had a rocket engine that the astronauts fired to begin circling the moon. 宇航员点燃服务舱的火箭发动机，可以开始绕月飞行。
- Hypergolic ignition systems bear many resemblances to hybrid rockets. 自然式点火系统在很多方面与混合型火箭相似。
- Numerical solutions of full Navier-Stokes equations with chemical reaction flow were established for the nozzle flow of the LOX/HTPB hybrid rocket motor. 利用二维轴对称N-S方程和组分方程对选用液氧/端羟基聚丁二烯推进剂的固液混合火箭发动机喷管流动进行了计算。
