推进技术 ›› 1996, Vol. 17 ›› Issue (5): 32-34.

• • 上一篇    下一篇

固体发动机内弹道计算软件包的实现

张为华,李清廉,侯中喜,王敏毅,石东风   

  1. 国防科技大学航天技术系;国防科技大学航天技术系;国防科技大学航天技术系;国防科技大学航天技术系;国防科技大学航天技术系
  • 发布日期:2021-08-15

REALIZATION OF SOFTWARE FOR SRM INTERIOR BALLISTIC CALCULATION

  1. Dept.of Aerospace,National Univ.of Defense Technology,Changsha,410073;Dept.of Aerospace,National Univ.of Defense Technology,Changsha,410073;Dept.of Aerospace,National Univ.of Defense Technology,Changsha,410073;Dept.of Aerospace,National Univ.of Defense Technology,Changsha,410073;Dept.of Aerospace,National Univ.of Defense Technology,Changsha,410073
  • Published:2021-08-15

摘要: 介绍了固体发动机内弹道计算软件包的组成、框架、结构及特点。该软件包全部采用C语言编写,在接口、数据结构、界面、移植性和扩展性等方面具有优势。

关键词: 固体推进剂火箭发动机;计算机辅助设计;内弹道计算;软件包

Abstract: The composition,structure and features of software for SRM for internal ballisticcalculation are introduced. The software is programmed in C language.It is practical and referred to SRM engineering design.

Key words: olid propellant rocket engine;Computer aided design;Interior ballisticcalculation;Software package