摘要
对导弹发射车的起竖机构做较全面的分析，提出了在解析法的基础上，用计算机设计起竖机构的方法。做到对不同设计方案进行快速比较和选择，提高了设计质量和效率。
The missile launcher erector structure is comprehensively analysed. On the basis of analytic method, the method of using computer to design erector structure is proposed. Different design projects are rapidly compared and chosen, and design quality and efficiency are improved.
出处
《导弹与航天运载技术》
1996年第1期16-25,共10页
Missiles and Space Vehicles
关键词
导弹
发射车
起竖机构
Guided missile launching,Force.
