Statistical analyses methodologies, such as analysis of variance, non-parametric tests and hypothesis tests were applied to uncover trends and dependencies of ejection-related injuries. Ejection-related fatality patterns for the A-6 aircraft were developed deterministically. The A-4, A-5, A-6, A-7, F-4, F-8 and F-9 ejection-related injuries were investigated, and parent probability density functions derived. The A-4, A-6, A-7, F-4 and F-8 contain an underlying injury trend. Fatalities occur randomly upon ejection from the A-4, A-7, F-4 and F-8 aircraft. Fatalities do not occur randomly from the A-6 aircraft. Differences were revealed among various ejection fatality scenarios: hardware hazards, aircrew judgment, environmental conditions, aircraft associated with ejections, and ejection seats used in ejection. (Author)
Statistical Analyses Applied to the U. S. Navy Aircrew Automated Escape Systems
1976
96 pages
Report
No indication
English
Aircraft , Escape systems , Flight crews , Aviation safety , Wounds and injuries , Ejection seats , Automation , Attack bombers , Jet fighters , Statistical samples , Analysis of variance , Nonparametric statistics , A-4 aircraft , A-5 aircraft , A-6 aircraft , A-7 aircraft , F-4 aircraft , F-8 aircraft , F-9 aircraft
Aircrew Automated Escape System Simulation Model
NTIS | 1974
|Attitude Selective Aircrew Escape Control
NTIS | 1978
|NTIS | 1964
|Laser sequencing for aircrew escape applications
AIAA | 1995
|