Accession Number:

ADA305654

Title:

Development of In Situ Stiffness Properties for Shuttle Booster Filament Wound Case

Descriptive Note:

Corporate Author:

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC

Personal Author(s):

Report Date:

1984-08-01

Pagination or Media Count:

59.0

Abstract:

Subscale tests were extensively used to develop a data base on elastic properties of graphite-epoxy wound pressure vessels. Scaling phenomena were observed to influence biaxial strains. Causes for scaling are proposed and lamina models with scaling factors are presented. MM

Subject Categories:

  • Laminates and Composite Materials
  • Solid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE