Accession Number:
AD0249771
Title:
STRUCTURAL TEST PROGRAM F-106A AIRPLANE
Descriptive Note:
Corporate Author:
WRIGHT AIR DEVELOPMENT DIV WRIGHT-PATTERSON AFB OH ENGINEERING TEST DIV
Personal Author(s):
Report Date:
1960-08-01
Pagination or Media Count:
72.0
Abstract:
The F-106 airplane was subjected to a complete static test program covering all of the critical flight, landing and ground handling conditions.
Descriptors:
Subject Categories:
- Attack and Fighter Aircraft