Viscoelastic Response of HTPB Based Solid Fuel to Horizontal and Vertical Storage Slumping Conditions and it's Affect on Service Life

Author:

Nawaz Qamar1,Nizam F.1

Affiliation:

1. Center of Excellence in Science and Applied Technologies

Abstract

Frequent use of solid fuels as thrust generating energy source in modern day space vehicle systems has created a need to assess their serviceability for long term storage under various conditions. Solid fuel grain, the most important part of any solid fuel system, responds viscoelastically to any loading condition. For the assessment of the service life of any solid fuel system, the solid fuel grain has to be structurally evaluated in applied storage conditions. Structural integrity of the grain is exceptionally significant to guarantee the successful operation of the solid fuel system. In this work, numerical simulations have been performed to assess the mechanical stresses and strains induced in an HTPB based solid fuel grain during service life employing ABAQUS standard FEA software using 4-node bilinear quadrilateral elements. For finite element analysis (FEA), typical 2-D and π/nthaxisymmetric section of 5-point (n) star grain geometry is considered. Mechanical loads include the horizontal or vertical 1-g (solid fuel weight) storage condition. The simulation results are compared with the analytical results for the same grain geometry. Analytically measured slump deflections in grain segment at various storage times have been found in good relation with the FEA based simulation results. This proves the validity of the procedure adopted and is helpful in assessment of the service life of solid fuel systems.

Publisher

Trans Tech Publications, Ltd.

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference22 articles.

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2. P. J. Blatz, W. L. Ko, and A. R. Zak, Fundamental studies relating to the mechanical behavior of solid propellants, rocket grains and rocket motors, Graduate Aeronautical Lab., California Institute of Technology SM62-63 (May 1962), pp.33-40.

3. L. R. Herrmann and M. Tamekuni, Horizontal Slump of Solid Propellant Motors, AIAA J. vol. 3/4 (1965), pp.696-700.

4. U. E. Garrison, Grain Stress Analysis Study, AD Report No. AD-893602 (Feb 1972).

5. J. E. Fitzgerald, Handbook for the Engineering Structural Analysis of Solid Propellants, University of Utah Lake City, Utah, (1971).

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