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Aircraft Survivability • Spring 2003 • http://jas.jcs.mil
Although susceptibility-reduction measures such as the installation of IRCM systems on airliners would no doubt improve the survivability of those aircraft, experience has shown that vulnerability reduction should not be overlooked. Simply focusing on the susceptibility side of military aircraft was not sufficient, and many pilots owe their safe return from hostile environments to vulnerability reduction efforts. Since no IRCM system is likely to prove 100 percent effective against all current and emerging IR missile threats, it may be wise to direct additional attention towards reducing civil aircraft vulnerability. Regardless of the measures used on any particular aircraft design—whether relying on such familiar approaches such as dispersing redundant critical components around the aircraft, armoring hydraulic lines, installing self-sealing fuel lines, and installing strategically-placed fuel shut-off valves, or whether one looks towards fuel tank fire and explosion protection through the use of powder panels or other technology, adjusting fuel chemistry to reduce the chances of fire or explosion, improved turbine blade and disk debris containment, or even adopting explosive-resistant and lightweight fuselage materials—focusing additional resources on vulnerability reduction should be a priority. An additional benefit that comes from vulnerability reduction efforts is that they also provide a degree of protection against non-IR threats such as RF missiles, RPGs, high-caliber machine guns and sniper rifles, as well as from damage caused by explosives that might slip through the passenger and baggage screening process. The efforts of the survivability community have resulted in the design of combat aircraft that are significantly more likely to avoid and survive MANPADS attacks. One notable example is the success of the F/A–18 Hornet during Desert Storm. The time may have come to apply aggressively the lessons learned in the military context to the civil air fleet. This will not likely be cheap and will in all likelihood necessitate live-fire testing with an assortment of commercial aircraft of different sizes and different propulsion systems. Whether such tests are conducted on static aircraft or whether additional funding can be obtained to “drone” the test aircraft, to avoid conducting live-fire testing based on cost considerations would be shortsighted. Regardless of the funding mechanism, arguments against such testing based on cost considerations are misplaced. Put that one in your pipe and smoke it brooks |
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