G Limits, how much G is enough: 7.5 or 9G capability?
On another note, out of curiousity, why are the latest carrier borne fighters not built for 9G turns. I understand that its not usually a capability that would be tactically useful since it bleeds energy so quickly, but it seems like something that might come in handy in certain situations like an evasive maneuver. Again it seems like the Air Force puts some value on this capability since the F-15, 16, and 22 are all stressed for 9G, and the CTOL F-35 apparently is too, while the CVN and STOVL F-35, as well as super hornets and legacy hornets are all limited in the 7-7.5G range. Is this a result of the Navy trying to extend the service life of its aircraft by shrinking the envelope artificially in the flight control computers? Or maybe it has to do with cutting weight in some areas that allows for the added weight necessary in others (i.e landing gear)? Just curious if anyone has insight on this. Also I've heard that hornets have a button on the stick that allows the pilot to tell the computer to max out the jet at 9 instead of 7.5, for emergencies. Anyone know if that is true? (If this is another OPSEC thing than nevermind)