Development of Ultra-High Strength Rocket Motor Cases by Cryogenic Stretch Forming and Cooled Solid Propellant Rocket Nozzles

摘要

This report gives an account of progress for the period December 21, 1960 to January 20, 1961. The information is presented in two (2) sections. The first section describes the work performed on Task A, Development of Ultra-High Strength Rocket Cases by Cryogenic Stretch Forming. The second section reports progress on Task B, Cooled Solid Propellant Rocket Nozzles.