1.
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
2.
nozzle diaphragm
喷管挡栅板 -固体火箭发动机的
3.
The Development of Integral Design of Solid Rocket Motor Nozzle;
固体火箭发动机喷管热结构CAD设计
4.
Numerical simulation of gas-particle flow in nozzle of solid rocket motor
固体火箭发动机喷管气固两相流动的数值模拟
5.
Investigation of Aft-End Internal Flows in Solid Rocket Motors with Submerged Nozzle;
固体火箭发动机潜入喷管背壁区流动研究
6.
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
7.
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
8.
Thermal and Thermal-Structural Couple Analysis of the Rosette Carbon-Carbon Nozzle in SRM;
碳/碳固体火箭发动机柔性喷管热及热－结构耦合作用研究
9.
The Particle Parameter and Temperature Measurement for the Wake of Solid Propellant Rocket Motor(SRM)
固体火箭发动机喷管出口粒子参数和尾流温度测量方法研究
10.
Upgrade the Performance of Single Combustion Chamber Dual Thrust SRM by Unilateralism Nozzle Throat Area Control
利用定向可调喷管提升单室双推固体火箭发动机性能
11.
CHANGEMENT OF SOLID ROCKET PLUME INFRARED SIGNAL WITH FLY PARAMETERS
固体火箭喷焰红外信号随飞行参数的变化
12.
Integrated numerical simulation and software implementation on two-phase flow field and structure temperature field of solid rocket motor nozzle
固体火箭发动机喷管两相流场与结构温度场一体化数值模拟与软件实现
13.
Four nozzles, canted outboard, split the exhaust of the solid rocket motor into four equal tails.
四个向外倾斜的喷管把固体火箭发动机的排气流分成四个相等的尾巴。
14.
Stress Field Analysis Near Crack Tip Buried in the Rosette Carbon-Carbon Nozzle of SRM;
固体火箭发动机花瓣铺层碳/碳柔性喷管扩张段裂尖附近应力场研究
15.
solid propellant binder
固体火箭燃料粘结剂
16.
solid Rocket Booster
固体燃料火箭助推器
17.
solid rocket system
固体燃料火箭动力装置
18.
A METHOD FOR DESIGN OF SMALL BEVEL NOZZLE OF ROCKET ENG INES
火箭发动机小斜切角喷管的设计方法