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.