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On Mon, 19 Jul 2004 16:30:14 +1000, John Cook
wrote: On Sun, 18 Jul 2004 07:29:56 -0600, Scott Ferrin wrote: On Sun, 18 Jul 2004 19:45:53 +1000, John Cook wrote: Ooops missed out the source for thwe !.5 Mach claim "Much is currently being made about supercruise, that is the ability to cruise supersonically without the use of reheat (afterburn) for extended periods of time. Although never stated explicitly (as for example with the U.S. F-22) the Typhoon is capable of and has demonstrated such an ability since early in its flight program according to all the Eurofighter partnets. Initial comments indicated that, with a typical air to air combat load the aircraft was capable of cruising at M1.2 at altitude (11000m/36000ft) without reheat and for extended periods. Later information appeared to suggest this figure had increased to M1.3. However even more recently EADS have stated a maximum upper limit of M1.5 is possible although the configuration of the aircraft is not stated for this scenario (an essential factor in determining how useful such a facility is). " Cheers John Cook Uh. . . you still missed the source :-). It sounds a lot like the Airtime Publishing blue book (Airpower somethin-or-other) that had the Typhoon for the focus aircraft a few years ago though. In it they mentioned that in turning the Eurofighter could outdo anything except the F-22 had better sustained turning at both subsonic and supersonic speed and better instantainious at high speed. The only area the Eurofighter was better according to the article was instantainious at subsonic speed. Yup your right, its at .65 M the Typhoons a tad better at instantaneous turn rate, not the 1.6 Mach where the F-22 is a tad better, the reference was on pages 95/96 of the World air power journal #35. Seems the F-22's Thrust vectoring really helps in the sustained rate!!. Cheers John Cook FWIW the Tomcat could do 7.5g at Mach 2.2 because of those little flip out canard-like things in the glove. They didn't even have to move, all they did was bump the center of pressure forward to offset the effect of increased stability brought on by the higher speed. |
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