Research for Attack Aircraft

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January 1, 1992
Effects of impinging gas from the AV-8B Short-Takeoff Vertical-Landing (STOVL) aircraft require that personnel remain 50 feet away during vertical operations. In future STOVL aircraft, vertical thrust will be greater, with a potentially larger danger area. This memorandum examines the factors that determine the size of the danger area and models the amount of area future STOVL aircraft will need.
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June 1, 1974
The kind of information that can be obtained from analysis of Aircraft Vulnerability Report Forms is described, and the results of a preliminary study, made to determine the value of a larger-scale analysis, are reported. The study concludes that: (1) although hits from ground fire are uniformly distributed over both jet and conventional aircraft, the jets received a greater proportion from ahead and directly below; (2) in terms of aircraft lost per hit, the F-4U is twice as vulnerable as the F-9F, which is in turn twice as vulnerable as the AD; and, (3) the variation in vulnerability among aircraft can be markedly affected by design.
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June 1, 1974
This paper develops an applied analytical model which can be used by Navy planners to predict the minimum cost pipeline planning factors for aircraft of a particular type, model, and series. The capabilities of the model are demonstrated with an actual analysis of the A-7 aircraft pipeline factor. The results are the determination of the optimal pipeline factor for the A-7 and its associated resource requirements and costs.
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June 1, 1970
Studies the relationship between aircraft readiness and spares usage at the squadron level, specifically for the F-4B, CH-53 and TA-4F. The study determines the best combinations of aircraft, maintenance man-hours, and spare parts for various budgets. Since the availability of spare parts is a big factor in aircraft readiness, a detailed examination was made of the spare parts resupply system, and recommendations are made for improving this system for decreasing the time it takes for a supply requisition to be filled. Additional recommendations are made for changing the current method of estimating the quantities of spare parts needed for a specific aircraft model.
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June 1, 1969
Documents the development of an applied model for planning pipeline aircraft procurement. Using the techniques of network analysis, the model is illustrated with the A-7 aircraft undergoing Progressive Aircraft Rework (PAR) at Naval Aircraft Rework Facility, Jacksonville. A range of pipeline factors for the A-7 is evaluated and suggestions are made for applying the model to other type, model, and series of aircraft.
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April 1, 1965

This study determines the effectiveness of various A-1 aircraft payloads against bridges. The optimum load, regardless of bridge type, consists of eight 500 pound bombs plus additional ordnance as permitted by radius, loading time, and weight considerations. The effects of different intervalometer settings and approach angles are also analyzed: effectiveness is reduced if long intervalometer settings are used, but is insensitive to approach angle if the optimum setting is used. Data for adjusting the effectiveness estimate to reflect variations in bridge size and delivery accuracy are also provided.

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December 1, 1964
The ballistic dispersion of low drag bombs dropped in sticks from the A-4 aircraft is calculated from test data. The data is inadequate to permit determination of whether dispersion depends on slant range or time of fall, but an estimate can be made for delivery parameters of interest.
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