Accession Number:

AD0605945

Title:

THERMAL GRAIN STRUCTURAL ANALYSIS

Descriptive Note:

Program progress rept. no. 13, 1-31 Dec 1962

Corporate Author:

LOCKHEED PROPULSION CO REDLANDS CA

Personal Author(s):

Report Date:

1962-12-31

Pagination or Media Count:

17.0

Abstract:

Effort was concentrated on computer determination of stresses in thermally cycled propellant grains. Parametric thermal stress data for grains with varying dimensions subjected to step thermal conditioning and the results of rapid cooling tests of analogue motors are presented.

Subject Categories:

  • Solid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE