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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.
- Defense Technical Information Center
Abstract: The report presents results of tests conducted...
- Defense Technical Information Center
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.
MK 7 AIRCRAFT RECOVERY EQUIPMENT. Present-day aircraft normally require the use of runways that are 5,000 to 8,000 feet long in order to land ashore. On an aircraft carrier, these same aircraft...
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.
By way of background, in 2003, the US Navy determined that the Mark 7 Mod 3/Mod 4(MK -7) arresting system being used to permit landings existing aircraft on carriers was approaching its design limit.
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.
