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Simply stated, aircraft performance is defined as how far, how fast, how high, and carrying what for how long to perform a specific task. Stated in the vernacular of the aircraft designer, these are range, speed, altitude, payload, duration and mission. Defining the performance of the A-7, or any other modern military aircraft, is a very complex task because there are so many variables, all interacting with each other. To simply state the maximum or minimum value of a performance element gives only the most general feel for the vehicle. The complexity of this issue is revealed by the Flight Handbook, USAF Technical Order 1A-7D-1, Section V, Operational Limitations, which requires 53 pages to define 34 stores (weapons and external fuel tanks) that can be loaded on the 68 store stations of the A-7 in 216 different configurations! Each of these configurations affects airspeed and acceleration (g-load) for carriage, employment, and release and jettison factors. Each configuration also affects dive angle, cg (center of gravity, range, total drag, total aircraft weight, and, in some cases, takeoff distance and maximum altitude. However, so that some comparison can be made of the different models in the A-7 family, we have taken the CLOSE AIR SUPPORT and SEARCH & SURVEILLANCE missions as examples. For each mission in the comparison, the payload is defined as 6 Mark 82 Low-Drag General Purpose bombs, 500 rounds of 20-mm ammunition, and a full fuel load.
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A-7: Genesis of the Navy Attack Bomber, Light (VA(L))
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