1.
Research on Key Technologies of Micro Solid Propellant Thruster;
微型固体火箭发动机设计与制造关键技术研究
2.
Numerical simulation of temperature fields of solid propellant micro-rocket with inner wall treated by PMAO techniques
内壁经微弧氧化处理的微型固体火箭温度场的数值模拟
3.
Design and Experiments of Aft-ignition for Small Solid Rocket Motor
小型固体火箭发动机尾部点火设计与实验
4.
FAILURE ANALYSIS OF THE MODEL SOLID ROCKET MOTOR CASE IN HYDROTEST
某型号固体火箭发动机壳体水压破坏分析
5.
solid propellant binder
固体火箭燃料粘结剂
6.
solid Rocket Booster
固体燃料火箭助推器
7.
solid rocket system
固体燃料火箭动力装置
8.
ANALYSIS ON RELIABILITY GROWTH FOR A CERTAIN SOLID ROCKET ENGINE
某型固体火箭发动机的可靠性增长分析
9.
Large eddy simulation of vortex shedding for model SRM
模型固体火箭发动机内涡脱落过程的大涡模拟
10.
A NEW METHOD TO REDUCE ABLATIVE HARM ON THROAT FOR SMALL ROCKET NOZZLE
减轻小型固体火箭喷管喉部烧蚀危害的新措施
11.
Analysis and Contrast of Numerical Simulation Models of Two-phase Flow in Solid Rocket Motor;
固体火箭发动机两相流计算模型分析与比较
12.
Study on Canted Scarfed Flow-backward Multi-nozzle SRM;
小型斜置倒流多喷管固体火箭发动机研究
13.
A New Type of Solid Rocket Engine Fuel--Paraffin-based Fuel
一种新型固体火箭发动机燃料——石蜡基燃料
14.
Real-time Monitoring System of Demoulding Device for Miniature Solid Rocket Motor
小型固体火箭发动机脱模实时监控系统的研制
15.
Pegasus is the first air launched solid rocket in America, which is used to place small satellites into low earth orbit.
飞马座火箭是美国第1种机载空中发射型固体运载火箭,主要用于将小型卫星送入近地轨道。
16.
Calculation method of microwave attenuation by exhaust plume of solid rocket motors
固体火箭发动机排气羽流对微波衰减的计算方法
17.
Establishment of Mechanical Model of High-speed and High-acceleration Solid Rocket Engine Case
高速高加速固体火箭发动机壳体力学模型的建立
18.
nozzle diaphragm
喷管挡栅板 -固体火箭发动机的