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固体发动机内弹道计算分析中的几个问题
引用本文:何景轩.固体发动机内弹道计算分析中的几个问题[J].固体火箭技术,1997,20(3):21-25.
作者姓名:何景轩
作者单位:中国航天工业总公司四院四十一所!西安,710025
摘    要:对固体发动机内弹道进行了分析,获得了喷喉面积和燃速的变化规律及燃面到肉厚的关系,同时阐述了内弹道性能计算分析了中有关问题。

关 键 词:固体火箭发动机  内弹道计算  燃速

Several Problems in Analysis and Calculation of the Interior Ballistics of Solid Rocket Motor
He Jingxuan.Several Problems in Analysis and Calculation of the Interior Ballistics of Solid Rocket Motor[J].Journal of Solid Rocket Technology,1997,20(3):21-25.
Authors:He Jingxuan
Abstract:The nozzle throat area and grain burning rate versus time, and grain burning surface area versus web are obtained by analyzing the interior ballistic of solid rocket motor. The problems in analysis and calculation of the interior ballistic of solid rocket motor are discussed.
Keywords:Solid propellant rocket engine Interior ballistic calculation Burning rate
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