thrust reversal

In this paper, a simple method for analysis of ground test data of the solid rocket motor with reversal nozzles is presented based on solving the reverse thrust at an altitude from ground test data.

文中介绍了根据地面实验数据分析反喷管在高空提供的反推力，为带反喷管发动机地面实验数据处理提供了简便的分析方法。

It's verified that a series of intense pressure impulses can occur in the combustion chamber after the thrust reversal nozzles of the solid rocket motor are suddenly opened.

实验表明，突然打开固体火箭发动机反向喷管后，燃烧室中可能出现强烈的压力冲击，这种压力冲击来自喷管喉部节流和形成准稳态流动之前的非定常过程。

A Unsteady Two-Phase Flow Model of Thrust Reversal

推力中止过程的两相流动数值模拟

Thrust reversal interference analyses of solid missile and measures for solving attitude disturbance of reentry body

固体导弹反喷干扰分析及再入体姿态扰动的解决措施

The paper discusses influence of the non-dimensional throat area of the reversal nozzle for thrust termination and the angle included between the axes of reversal nozzle and rocket motor on the propellant weight for cutout.

本文讨论反喷管相对喉面、反喷管轴线倾角对关车药量的影响以及关车药量的计算方法。

Technique of thrust termination with reversal nozzle for solid rocket motors

固体火箭发动机反向喷管推力终止技术