1.
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
2.
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
3.
The Research on Characteristic Performance of Combustion Flow Field in Secondary Combustion Chamber for Extended Range Solid Rocket Ramjet
增程固体火箭冲压发动机补燃室燃烧特性研究
4.
Predominance of Ducted Solid Rocket Ramjet Applied to Airborne Missile
固体火箭冲压发动机在空空导弹上应用的优势
5.
Research on the Secondary Combustion Chamber Operation Process of Boron-Based Propellant Ducted Rockets;
含硼推进剂固体火箭冲压发动机补燃室工作过程研究
6.
Three-Dimensional Numerical Simulation of Afterburner Flow Field of Solid Rocket Ramjet
固体火箭冲压发动机补燃室流场三维数值计算研究
7.
Research on Thermal Protecting of Afterburning Chamber for Integral Solid Rocket-ramjet
固体火箭冲压发动机补燃室梯度热防护体系研究
8.
Study on theoretical performance of solid ducted rocket based on thermodynamic calculation
基于热力计算的固体火箭冲压发动机理论性能研究
9.
Effects of Jet Rotational Angle on the Second Combustor of Boron-based Propellant Solid Rocket Ramjets
含硼固体火箭冲压发动机中燃气旋流角对补燃室的影响
10.
turbo-ram rocket engine
涡轮冲压式火箭发动机
11.
Characteristics tests of pulse liquid rocket engine with high chamber pressure
高室压脉冲液体火箭发动机特性试验
12.
Aerodynamic Design of Turbo for Solid Rocket Turbo Ramjet Engine;
固体火箭涡轮冲压发动机涡轮气动设计
13.
Study on the characteristics of bipropellant-fueled pulse rocket engine with high combustion chamber pressure
双组元高室压脉冲火箭发动机工作特性分析
14.
Experimental Research on Performance of Pulse Detonation Rocket Engine;
脉冲爆震火箭发动机性能的实验研究
15.
Experimental investigation of the pulse detonation rocket engines with variable cross-section
变截面脉冲爆震火箭发动机实验研究
16.
The rockets give the planes and missiles enoughspeed to make the ramjet engine workable.
这种助推火箭为飞机和导弹提供足够的速度，以使冲压式喷气发动机可以开动工作。
17.
Analysis of Shock Response Spectrum for Liquid Rocket Engines
液体火箭发动机冲击响应谱分析计算方法
18.
Numerical simulation for tank pressurization system of LRE test-bed
液体火箭发动机试验台贮箱增压系统数值仿真