发射动力系统内弹道优化设计计算  

Interior trajectory optimization design and computation of launching power system

作　　者：陈庆贵[1] 齐强[1] 周源[1] 赵汝岩[1] 

机构地区：[1]海军航空工程学院,山东烟台264001

出　　处：《舰船科学技术》2011年第5期91-93,97,共4页Ship Science and Technology

摘　　要：建立了燃气-蒸汽发射动力系统内弹道优化设计的基本关系式,并对某型导弹的弹射内弹道进行了设计计算。计算结果与试验结果相吻合,对弹射内弹道的工程设计具有一定的参考价值。Basic relation formulas for gas-steam launching power system interior trajectory design were established,and ejecting interior trajectory of one missile was computed.The results were in accordance with that of experiment.It was of some reference value for the engineering design of ejecting interior trajectory.

关 键 词：燃气-蒸汽发射动力系统 弹射内弹道 冷发射 

分 类 号：TJ02[兵器科学与技术—兵器发射理论与技术]