Accession Number:

AD0654042

Title:

STRESS ANALYSIS MAIN LANDING GEAR

Descriptive Note:

Corporate Author:

GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT

Personal Author(s):

Report Date:

1964-01-01

Pagination or Media Count:

231.0

Abstract:

The report consists of data substantiating the structural integrity of the main landing gear shock strut.

Subject Categories:

  • VSTOL
  • Research and Experimental Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE