底排-火箭复合增程技术中最佳底排质量流率方案的确定方法

The Method Decided of Best Base-Bleed Mass Flowing Ratio Scheme in the Technique of Base Bleed-Rocket Compound Assistant Range

文中对底排 -火箭复合增程弹的底排质量流率最佳方案给出了相应的算法和典型结果 ,同时该算法还可同步给出对火箭发动机的冲量要求 ,本算法和结果将有助于 1 55m m口径底排

In this paper, the corresponding arithmetic and typical results are given to the base bleed mass ratio optimization scheme on the base bleed rocket compound long range shell. The arithmetic also given require of rocket motor's impulse in phase. The arithmetic and results will be helpful to the designing and analysis of large caliber shell with base bleed rocket compound assistant range technology.