DEVELOPMENT OF HIGH PERFORMANCE ROCKET MOTOR CASE
Quarterly engineering progress rept. no. 18, 1 Oct-31 Dec 1961
BUDD CO PHILADELPHIA PA
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Design drawings were completed for the 20 in. diameter test chamber in the development of a solid rocket motor case. Two alloys, Ti-13V11Cr-3Al alloy and 20 nickel steel having 1.7 Ti and 0.5 Al, were selected as the fabricating materials. Manufacturing of the cases was begun. Welding tests were continued.
- Solid Propellant Rocket Engines