Accession Number:

AD0436272

Title:

IMPROVED FILAMENT-WOUND CONSTUCTION FOR CYLINDRICAL PRESSURE VESSELS, VOLUME 1. STRUCTURAL ANALYSIS AND MATERIALS AND PROCESSES

Descriptive Note:

Rept. for 1 July 1961-31 Jan 1964

Corporate Author:

AEROJET-GENERAL CORP AZUSA CA

Personal Author(s):

Report Date:

1964-03-01

Pagination or Media Count:

226.0

Abstract:

A design-optimization program was conducted that included stress analyses and the determination of design parameters, winding patterns, and fabrication techniques for filament-wound, cylindrical, pressure vessels. An investigation of the materials, processes, and structural analyses required to efficiently utilize the improved mechanical properties of new glass fibers was also conducted, with the aim of improving filament-wound composite structures.

Subject Categories:

  • Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE