Published February 1962 | Version Submitted
Technical Report Open

Fundamental Studies Relating to the Mechanical Behavior of Solid Propellants, Rocket Grains and Rocket Motors

Abstract

The former reports provided considerable information about foam and continuum rubbers under three types of tensile loading (i.e. uniaxial, strip-biaxial and homogeneous-biaxial tension). Since continuum rubbers are almost incompressible it is extremely difficult to determine the strain energy function beyond the linear term. On the other hand the highly dilatable foam rubber enables one to determine the functional form of the strain energy valid up to higher order terms. Special attention is being paid to foam rubber, since it represents .the limiting case of completely dewetted propellant. The present report will (i) furnish the method of determination of strain energy function and the associated constitutive stress-strain law for large deformations out to fracture and (ii) present the triaxial tensile test data needed to double check item (i).

Additional Information

GALCIT 118 A - Progress Report No. 3 Aerojet Contract S-4200061-OP November 28, 1961 - February 28, 1962. This program is being supported by the Aerojet-General Corporation, Sacramento Division, under technical cognizance of Dr. F. J. Climent to provide technical support to the Polaris Project.

Attached Files

Submitted - Fundamental_Studies_Relating_to_the_Mechanical_Behavior_of_Solid_Propellants.pdf

Files

Fundamental_Studies_Relating_to_the_Mechanical_Behavior_of_Solid_Propellants.pdf

Files (6.9 MB)

Additional details

Identifiers

Eprint ID
62588
Resolver ID
CaltechAUTHORS:20151203-152918001

Funding

Aerojet-General Corporation
S-4200061-OP

Dates

Created
2015-12-04
Created from EPrint's datestamp field
Updated
2021-11-23
Created from EPrint's last_modified field

Caltech Custom Metadata

Caltech groups
Graduate Aeronautical Laboratories (Solid Mechanics) , GALCIT
Other Numbering System Name
GALCIT Report SM
Other Numbering System Identifier
62-14