Accession Number : AD0433055


Title :   WEAPON SYSTEM 107A-2 PRODUCT ENGINEERING PROGRAM. COATED METALLIC THRUST CHAMBERS EXPANDABLE NOZZLES COMBUSTION INSTABILITY SCALING CONCEPTS ABLATIVE THRUST CHAMBERS.


Descriptive Note : Monthly progress rept., 1-29 Feb 64.


Corporate Author : AEROJET-GENERAL CORP SACRAMENTO CALIF


Report Date : 15 Mar 1964


Pagination or Media Count : 30


Descriptors :   *LIQUID PROPELLANT ROCKET ENGINES , THERMAL INSULATION , ROCKET NOZZLES , HIGH TEMPERATURE , QUALITY CONTROL , TETROXIDES , PERFORMANCE(ENGINEERING) , REGENERATIVE COOLING , THRUST , STABILITY , ABLATION , FILM COOLING , HYDRAZINES , LIQUID ROCKET PROPELLANTS , PRODUCTION , PROCESSING , BOUNDARY LAYER


Distribution Statement : APPROVED FOR PUBLIC RELEASE