火箭增程弹

零风偏反坦克火箭增程弹的散布分析

Analysis of the Zero-wind Deviation from the Trajectories for Rocket-Assisted Anti-Tank Projectiles

火箭增程弹的扰动运动理论及其应用

Theory and Application of Disturbed Motion of Rocket-Assisted Projectiles

火箭增程弹多普勒雷达测速数据处理方法的研究

The Study of the Data Processing Method of Measuring Velocity from Doppler Radar for the Rocket-Assisted Cartridge

该方法可以用于火箭增程弹多普勒雷达测速数据处理。

The method can be used to deal with measuring velocity from Doppler radar of the rocket-assisted cartridge .

底排-火箭复合增程弹多元弹道模型

The Model of a Multiple Trajectory for a Hybrid 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

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

通过分析结果，对底排火箭复合增程弹的设计优化工作起到了重要的指导作用。

The results of the analysis has played an important role in the design and optimization works .

底排火箭复合增程弹射程影响因素及其规律性研究

The Studies on the Influencing Factors and Regularity of Extended Range Effectiveness for Hybrid Base-bleed-rocket Extended-range Projectile

本文以底排&火箭复合增程弹总体理论及其应用为主要研究内容。

The overall theory and application about a hybrid base-bleed-rocket extended-range projectile is studied in this paper .

底排火箭复合增程弹弹道参数匹配方案研究

The Study on Optimized Exterior Ballistic Parameter Matching Scheme of Hybrid Range Enhanced Shell with Base bleed and Rocket

结果将有助于某型号底排-火箭复合增程弹的设计分析。

The results will be useful to the design of Base - Bleed and Rocket Compound Extended Range Projectiles .

某型火箭增程破甲弹发动机弹道炸分析与处理

The analysis and treatment of the ballistic explosion in the engine of a certain rocket destroy - armour bomb

计算结果所揭示的规律性对底排火箭复合增程弹的工程研制具有较好的应用价值。

The research results could be effectively applied to improve the engineering development of a hybrid base-bleed-rocket extended-range projectile .

随着底排&火箭复合增程弹的发展，对固体火箭发动机在高速旋转条件下工作性能的要求越来越高。

Technology advancements in Base-bleed and Rocket Combined Improved Range Projectile have led to demanding requirements for the working performance of solid propellant rocket engine .

空中点火机构动态延期时间研究是底排&火箭复合增程弹实现其最佳增程弹道，提高最大射程密集度的重要环节。

Research on the dynamic delay-time of Hybrid igniting-device in the air is the basis of implementing it 's the best trajectory and improving its max cannon-shot denseness .

底排一火箭复合增程弹火箭空中点火延时机构延期时间的控制对于最大限度发挥火箭增程效率有着极其重要的作用。

It is very important that the extended range effect is improved farthest by being master of the dynamic delay time of a rocket - portfire in the air .

对火箭增程破甲弹的底部施加压力，求出弹内各部件的应力、应变分布情况，以此为研究依据，分析其结构是否合理。

The pressure is applied to the bottom of the cannonball , the stress and strain distribution of each component can be got by the analysis of Finite Element Method , then judging whether the structure is reasonable .