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#11
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![]() Yeah but of the three companies producing fighters it was the closest to finishing up production. Grumman didn't have anything in the pipeline after the Tomcat and where at this point in the ATF program NATF was still a consideration Grumman would seem to be a shoe-in if they were just interested in keeping the manufacturers going. Come to think of it one of the reasons the F-22 was chosen over the F-23 was because of the NATF requirement. Lockheed had planned a swing-wing F-22 for the carrier requirement. Not likely. ![]() In fact, the finite element analysis that the F-22 was built off of renders your comments laughable, Ferrin. Sorry but it's pretty much common knowledge Tarver. The fact that a self-claimed expert like yourself has never heard of it really makes me question your claim. http://www.aerospaceweb.org/question/planes/q0132.shtml To go from supplying the USAF with their premier fighter for the last forty or so years (F-4/F-15) to placing FIFTH in the competition to build a new fighter suggests that though the USAF wanted it all, aerodynamic performance took a distant second place behind stealth. Son, let me tell it like it is, when you take it down the road from number one you get less, not more. ???? Less *what*? Performance? It was number one on the F-15 and nobody who's flown the F-22 will give the nod to the F-15 when it comes to flight performance vs. the F-22. If the avionics stay lit and the tails doesn't delaminate on the F-22. The F-15 also had problems with delamination. What? The F-15 had the same kind of delamination problems with the horizontal tail that has popped up with the F-22. Any idea what airframe number they implimented the fix in on the F-22? Or is it still on the to-do list? AV-19 is supposed to be fixed, but there is no way for anyone to know that. |
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