Accession Number:

ADA301816

Title:

Time-Temperature-Stress Capabilities of Composite Materials for Advanced Supersonic Technology Applications.

Descriptive Note:

Monthly progress rept. no. 49, 1 Jul-1 Aug 77,

Corporate Author:

GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Personal Author(s):

Report Date:

1977-08-01

Pagination or Media Count:

8.0

Abstract:

Two doubler bond failures have occurred in the unidirectional BA1 flight simulation specimens. New doublers will be attached, and the specimens will be returned to test. The residual strength testing of the Phase I BE and GE flight simulation specimens and the specimen configurations are discussed. Quality assurance testing of the full size GPI Phase II panel was completed and results are presented. In the screening test portion of the new material evaluation full size panels of HT-SPMR-15 and HT-S710 have been fabricated and submitted for quality assurance testing.

Subject Categories:

  • Laminates and Composite Materials
  • Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE