plug nozzle

Cold-flow tests on 1-cell 2D linear plug nozzle

单元二维直排塞式喷管冷流实验

Thrust vector control for solid plug nozzle based on secondary injection

固体塞式喷管二次喷射推力矢量控制

The hot fire and cold flow experiments of two kinds of test plug nozzle engines were done to know more about the influence of plug nozzle performance by changing the angle of the primary nozzle.

为分析主喷管角度对塞式喷管性能的影响，对两种塞式喷管实验发动机进行了热试和冷流试验。

Colorful and Print smooth and efficient water-resistant, does not plug nozzle.

色彩艳丽、打印流畅、快干耐水 、 不堵塞喷头.

A system configuration of tripropellant rocket engine with linear plug nozzle

一种三组元直排塞式喷管发动机系统方案

Numerical analysis for thermal distortion in the plug of regenerative cooling plug nozzle

再生冷却塞式喷管塞锥热变形数值分析

To know more altitude compensation and base characteristics of plug nozzle, cold-flow tests on 1-cell 2D linear plug nozzle, which utilize high pressure air as propellant were conducted.

为研究塞式喷管的高度特性和底部特性，采用高压空气为工作介质对单元直排塞式喷管进行实验。

The results indicate that the performance of plug nozzle can be increased 2%~ 7% without base wall at low altitude.

实验结果表明：无底部盖板可提高塞式喷管低空性能2%~7%；