首页> 美国政府科技报告 >Development of Contoured Interlocking Tape Wound Titanium Rocket Motor Cases. Part 1. Design, Metallurgy and Experimental Fabrication.
【24h】

Development of Contoured Interlocking Tape Wound Titanium Rocket Motor Cases. Part 1. Design, Metallurgy and Experimental Fabrication.

机译:轮廓联锁带缠绕钛火箭发动机箱体的研制。第1部分。设计,冶金和实验制造。

获取原文

摘要

The development of pressure vessels for use in solid fuel rocket motor cases has reached a state wherein further progress may be restricted by lack of suitable high strength metals and limitations in methods of fabrication. Though the potentially high strength to weight ratio of fiber reinforced cases is recognized, the use of metallic cases offers certain advantages peculiar to metals alone. The objectives of the present contract consisted primarily of the development of fabrication and metallurgical procedures for the manufacture of two basic structural shapes, the development of a wrapping machine and finally the experimental manufacture of two sub-scale vessels. These objectives have been met. (MM).

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号