Αποτελέσματα Αναζήτησης
Failure data obtained during tests with the Mark 7 Mod 3 arresting- gear system was used to determine reliability by two methods: First, by finding an empirical relationship between total number of failures and service life and then deriving the functional relationship of reliability to service life and mission size.
The report presents results of tests conducted with the Mark 7 Mod 3 arresting gear to determine aircraft compatibility and evaluate arresting-gear performance. Instrumented A-3A, A-4B, F-4A, and F-8D aircraft were utilized in the test program.
Failure data obtained during tests with the Mark 7 Mod 3 arresting-gear system was used to determine reliability by two methods: First, by finding an empirical relationship between total number of failures and service life and then deriviag the functional relationship of reliability to service life and mission size.
This report presents information regarding flight deck arresting gear and barricade configuration criteria for the Mark 7 Mod 3 arresting engines and is provided for use in the preparation of installation plans for new aircraft carriers or on present carriers planning utilization of the Mark 7 Mod 3.
The report presents results of tests conducted with the Mark 7 Mod 3 arresting gear to determine aircraft compatibility and evaluate arresting-gear performance. Instrumented A-3A, A-4B, F-4A, and F-8D aircraft were utilized in the test program.
Abstract : Failure data obtained during tests with the Mark 7 Mod 3 arresting- gear system was used to determine reliability by two methods: First, by finding an empirical relationship between total number of failures and service life and then deriving the functional relationship of reliability to service life and mission size.
Abstract : The report presents results of tests conducted with the Mark 7 Mod 3 arresting gear to determine aircraft compatibility and evaluate arresting-gear performance. Instrumented A-3A, A-4B, F-4A, and F-8D aircraft were utilized in the test program.
