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.
Development of Ultra-High Strength Rocket Motor Cases by Cryogenic Stretch Forming and Cooled Solid Propellant Rocket Nozzles
1961
32 pages
Report
No indication
English
ROCKET CASES , STRETCH FORMING , ROCKET MOTOR NOZZLES , COOLING , CRYOGENICS , PRESSURE , WELDING , FAILURE (MECHANICS) , STAINLESS STEEL , AUSTENITE , NIOBIUM ALLOYS , ALUMINUM ALLOYS , ROCKET MOTORS (SOLID PROPELLANT) , FILM COOLING , COOLANTS , LITHIUM , MOLYBDENUM , INJECTORS , LIQUID METAL COOLANTS , SPRAYS , STORAGE TANKS , STAINLESS STEEL 301 , SPRAY COOLING
Status of Cryogenic Solid Rocket Propellant Development
British Library Conference Proceedings | 2003
|NTIS | 1973
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