Accession Number : ADA313586
Title : SRM Propellant and Polymer Materials Structural Test Program.
Descriptive Note : Technical paper,
Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION HUNTSVILLE AL GEORGE C MARSHALL SPACE FLIGHT CENTER
Personal Author(s) : Moore, Carleton J.
PDF Url : ADA313586
Report Date : MAY 1988
Pagination or Media Count : 16
Abstract : The SRM propellant and polymer materials structural test program has potentially wide application to the testing and structural analysis of polymer materials and other materials generally characterized as being made of viscoelastic materials. The test program will provide a basis for characterization of the dynamic failure criteria for Solid Rocket Motor (SRM) propellant, insulation, inhibitor, and liners. This experimental investigation will also endeavor to obtain a consistent complete set of materials test data. This test data will be used to improve and revise the presently used theoretical math models for SRM propellant, insulation, inhibitor, liners, and seal O-rings.
Descriptors : *MATERIALS, *POLYMERS, *STRUCTURAL ANALYSIS, *SOLID PROPELLANT ROCKET ENGINES, MATHEMATICAL MODELS, EXPERIMENTAL DATA, MODELS, DYNAMICS, VISCOELASTICITY, FAILURE, SEALS(STOPPERS), O RINGS.
Subject Categories : Polymer Chemistry
Solid Propellant Rocket Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE