projectile-shaped rocket

At first the ballistic model of rocket projectile vertical launch is established, then it researches lift-to-drag ratio and influence of the angle of flight path on the firing range.

首先建立了火箭弹垂直发射的弹道模型，然后研究了升阻比、弹道倾角等参数的变化对火箭弹射程的影响，并分别对这两种情况进行了仿真。

The paper research fire angle of the projectile, firing time of the rocket motor, assisted time of the rocket motor, flying attitude of the glide phase and the terminal phase guidance law to add the projectile firing range.

在建立的模型的基础上，深入研究了炮弹的射角、火箭发动机的点火时间、火箭发动机的助推时间、滑翔段的飞行姿态以及末段制导律等对炮弹的射程及性能的影响。

Structural integrality analysis of rocket grain of base Bleed-Rocket compound extended range projectile

底排火箭复合增程弹助推火箭推进剂结构完整性分析

Comparative Analysis of Several Types of Igniter for Rocket Projectile

几种火箭弹点火具的对比研究

The Analysis of the Ballistic Trajectory Characteristics of A Short-Range Rocket Projectile under Impulse Control

火箭脉冲矢量控制弹道特性分析