Accession Number : AD0479227


Title :   SYSTEM SUPPORT STUDIES UNDER PRODUCTION SUPPORT PROGRAM. VOLUME 2. PART 1.


Descriptive Note : Final rept. 18 Aug 64-30 Sep 65,


Corporate Author : AEROJET-GENERAL CORP SACRAMENTO CA


Personal Author(s) : Childres, H E


Report Date : 30 Sep 1965


Pagination or Media Count : 141


Abstract : Contents: Study of TVC System Pressurization Methods; Nozzle-Motor Configuration Optimization; Motor Development, Layout, and Analysis; Bladder Improvement Study; LITVC Manifold and Joint Design Study; Investigation of Exit Cone Material Behavior; Igniter Initiator Materials-and-Performance Evaluation; Characterization of Pyrotechnic Ignition Properties; Evaluation of Alternative Insulation Materials; Roll-Control Valve Transducer Testing.


Descriptors :   *ROCKET NOZZLES , *SECOND STAGE ENGINES , RELIABILITY , WEIGHT , SURFACE TO SURFACE MISSILES , THRUST VECTOR CONTROL SYSTEMS , GUIDED MISSILE COMPONENTS , SOLID PROPELLANT ROCKET ENGINES , NOZZLE THROATS , NOZZLE GAS FLOW , SECONDARY INJECTION , THERMAL INSULATION , NOZZLE CLOSURES , NOZZLE INSERTS , PERFORMANCE(ENGINEERING) , GRAPHITE


Subject Categories : Liquid Propellant Rocket Engines


Distribution Statement : APPROVED FOR PUBLIC RELEASE