1)variable thrust pintle SRM喉栓式变推力固体火箭发动机
1.Internal ballistic regulating property of variable thrust pintle SRM喉栓式变推力固体火箭发动机内弹道调节特性
英文短句/例句
1.Internal ballistic regulating property of variable thrust pintle SRM喉栓式变推力固体火箭发动机内弹道调节特性
2.Experimental investigation of erosion performance of pintle in thrust-controllable SRM变推力固体火箭发动机喉栓烧蚀试验研究
3.Numerical analysis on dynamic response characteristics of pintle-controlled solid rocket motor喉栓式推力可调固体火箭发动机动态响应特性数值分析
4.Principle Experimental Research on Variable Thrust Pintle Motor;喉栓式变推力固体发动机原理试验研究
5.Investigation of ring aerodynamic throat for solid rocket motor固体火箭发动机环缝式气动喉部研究
6.Numerical Simulation of Inner Flow Field of a Pintle Injector Variable Thrust Rocket Engine针栓式变推力火箭发动机内流场数值仿真研究
7.Analysis on response of pressure in non-coaxial variable thrust pintle motor非同轴式喉栓变推力发动机压强响应分析
8.Thermodynamic cycle analysis on solid propellant air-turbo-rocket固体推进剂吸气式涡轮火箭发动机的气动热力循环分析(英文)
9.The Solid Rocket-Ramjet Engine Thrust Calculation and Experimental Research of Connected-Pipe Testing;固体火箭冲压发动机推力计算与实验研究
10.Simulation and Experiment of Thrust Performance for Solid Rocket Motor with Angle-cut Nozzle斜切喷管固体火箭发动机推力特性仿真与试验
11.Numerical Simulation of Flow in Variational Section of Segmented Solid Rocket Motor;变截面组合式固体火箭发动机内流场计算
12.Allan J.McDonald, "Design evolution of the space shuttle solid rocket motors"航天飞机固体火箭发动机的设计演变
13.dual thrust rocket engine双级推力火箭发动机
14.Study on the Measuring Technique of Thrust Line of Solid Rocket Motor with Laser Tracker;基于激光跟踪仪的固体火箭发动机推力线测量技术研究
15.Preliminary experimental investigation on small-thrust long-time working solid rocket motors小推力长时间工作固体火箭发动机初步试验研究
16.Numerical Study on Flow Control and Combustion Process of Variable Thrust Liquid Propellant Space Rocket Engine;空间变推力液体火箭发动机流量调节及燃烧过程仿真研究
17.The Development of Recycled Cooling Liquid Rocket Engine Combustion Chamber Design CAD System;再生冷却式液体火箭发动机推力室设计CAD技术研究
18.An Application Research of Integral Sol id Propellant Rocket Ramjets整体式固体火箭冲压发动机的应用性能探讨
相关短句/例句
pintle-controlled solid rocket motor喉栓式推力可调固体火箭发动机
1.Numerical analysis on dynamic response characteristics of pintle-controlled solid rocket motor喉栓式推力可调固体火箭发动机动态响应特性数值分析
3)pintle controlled solid rocket motor喉栓式固体火箭发动机
1.Numerical simulation of the flow field inside pintle controlled solid rocket motor was performed.对喉栓式固体火箭发动机内流场进行了稳态数值模拟,分析了喉栓头部型面、喉栓尺寸、喉栓位置对发动机性能的影响规律,结果表明发动机效率受喉栓头部型面、尺寸、位置等因素影响显著,所提供的结论可为喉栓式变推力固体火箭发动机的设计、试验及应用提供参考依据。
4)variable thrust liquid rocket engine变推力液体火箭发动机
1.The design and realization of a variable thrust liquid rocket engine control system is present in this paper.本文讨论了某型变推力液体火箭发动机数字控制系统的设计和实现。
5)solid propellant rocket motor固体推进剂火箭发动机
6)solid propellant rocket engine固体推进剂火箭发动机
1.The plume temperature is an important parameter, for solid propellant rocket engines and it is useful for determining the combustion process of the engine.推进剂的羽焰温度是固体推进剂火箭发动机的重要参数,对于研究发动机内的燃烧过程具有重要价值。
延伸阅读
固体火箭发动机 见导弹推进系统。
