摘要
文中以碳纤维增强树脂基复合材料研制导弹发射器为目的,通过对发射筒的结构和性能要求分析,提出碳纤维应用的必要性。介绍了碳纤维/玻璃纤维连续纤维缠绕研制导弹发射筒的成型工艺方法、性能试验手段和必要的试验数据。该研究成果已经成功地应用于某型号多用途导弹武器系统,为碳纤维在制导兵器结构部件上的应用提供技术支撑。
This paper aims at development of the missile launcher with carbon fiber reinforced resin matrix composite.The application necessity of carbon fiber is pointed out on the basis of analysis on the structure and performance requirement of the launch tube.This paper gives introduction for the forming technology of the launch tube by means of the development method of carbon fiber/fiberglass continuous winding,as well as performance test means and test data.The research result has been successfully used in a type of multi-purpose missile weapon system,providing technical support for use of carbon fiber in structural components of guidance weapons.
出处
《弹箭与制导学报》
CSCD
北大核心
2012年第1期9-12,共4页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
碳纤维
复合材料
混杂缠绕
导弹发射器
透湿率
carbon fiber
composite
hybrid winding
missile launcher
moisture permeability
