Accession Number : ADP006020
Title : Design and Analysis of Solid Rocket Motor Internal Insulation,
Corporate Author : EUROPEAN SPACE AGENCY PARIS (FRANCE)
Personal Author(s) : Truchot, A.
Report Date : APR 1988
Pagination or Media Count : 13
Abstract : The main purpose of internal insulation is to protect the motor case from the thermal environment of propellant combustion products. Several secondary objectives must also be met. Internal insulation must bond to propellant and case, transmit case strain into propellant and sometimes seal the case. In the first step, the general process of internal insulation design is presented: evaluation of thermal environment, selection of material, thermal and structural analyses. For each phase the different analysis methods are described: aerodynamic, thermal, and structural. The different phases of internal insulation fabrication are also presented: elastomer formulation, fabrication of parts and integration into the motor case.
Descriptors : *THERMAL INSULATION, *ROCKET ENGINE CASES, *ROCKET PROPELLANT GRAINS, INTERNAL, CASE BONDING, SOLID ROCKET PROPELLANTS, BONDING, ELASTOMERS, SELECTION, THERMAL PROPERTIES, MECHANICAL PROPERTIES, RUBBER, THERMAL ANALYSIS, STRUCTURAL ANALYSIS, FABRICATION, SOLID PROPELLANT ROCKET ENGINES, FRANCE.
Subject Categories : Solid Propellant Rocket Engines
Solid Rocket Propellants
Distribution Statement : APPROVED FOR PUBLIC RELEASE