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Fighter Combat - Tactics and Maneuvering

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One-versus-One<br />

<strong>Maneuvering</strong>,<br />

Dissimilar Aircraft<br />

Dissimilar fighters are fighters that have some performance characteristics<br />

which differ from those of the opponent by more than about 10<br />

percent. The performance measures of most interest are turn performance<br />

(both instantaneous <strong>and</strong> sustained) <strong>and</strong> energy performance (climb, acceleration,<br />

<strong>and</strong> speed). Of course there are many other ways in which fighters<br />

may differ (e.g., roll <strong>and</strong> pitch performance, size, pilot visibility limits,<br />

combat endurance, <strong>and</strong> radar capabilities). The influence of some of these<br />

factors is also discussed when appropriate.<br />

As explained in the Appendix, instantaneous turn performance is determined<br />

primarily by the ratio of aerodynamic lift to aircraft weight at low<br />

speeds (i.e., below corner velocity) <strong>and</strong> by the ratio of structural strength to<br />

aircraft weight at high speeds. Except in cases of extreme disparity in<br />

structural strength between fighters (i.e., on the order of a 50 percent<br />

advantage in maximum structural G for one aircraft), this limit is not<br />

usually as important in air combat as the aerodynamic limit. When a<br />

fighter pilot finds himself in a serious defensive situation, <strong>and</strong> to some<br />

extent when he is very near a lethal offensive position, he will use whatever<br />

G is required to save himself or to get the shot. A few popped rivets or<br />

some wrinkled skin is a small price to pay for the pilot's life or for a downed<br />

enemy aircraft. Since World War I there have been very few instances when<br />

a pilot has actually pulled the wings off his own fighter. Limits of structural<br />

strength must be adhered to in peacetime, however, since overstresses<br />

result in additional maintenance time, expense, <strong>and</strong> lost training.<br />

Therefore, ways must be found of winning within the design limits of the<br />

aircraft.<br />

The relative low-speed instantaneous-turn-performance capabilities of<br />

two fighters can be determined by comparing their velocity-load factor<br />

(V-n) diagrams (see the Appendix). The aircraft with the greatest usable G<br />

capability at a given speed has superior instantaneous turn performance<br />

(i.e., faster turn rate <strong>and</strong> smaller radius) at that speed. This G capability

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