bd popeye said:I don't know why you gents keep guessing about the F-22 Raptor. Just look it up on the USAF page.
Why bother with boring facts when one can speak right out one´s ass ???
bd popeye said:I don't know why you gents keep guessing about the F-22 Raptor. Just look it up on the USAF page.
Why bother with boring facts when one can speak right out one´s ass ???
Yes, the difference is the Raptor's radar is active. the Spirit's radar doesn't shoot anything, but the Raptor's do.BrotherofSnake said:Actually, the B-2 uses a AN/APQ-181 radar. The radar uses a passive, two dimensionally scanned antenna. It is the stealthiest radar in the world and it allows the B-2 to penetrate sophisticated air defenses while searching for targets.
I heard a Raptor can go much faster, but I guess they governed the engines or something, like what they did on the Abrams.
Two stages of burners next to each other? I doubt so. That'll waste a lot of fuel.Akula said:Comparing this F-119 to RD-33, i've studied closely, i do not see any major diffirerence in turbine scheme (except that compressor's shape is undoubtably more clever, and designed to lower aerodynamic resistance, but this will go for any 5th generation engine, i believe; oh, and of course it's controlling unit is more advanced), but engine has some mods, thats for sure. First - it does not seem to have afterburner at all (correct me if im wrong), Second - it's compressor's division degree (not sure how to call this paramater properly) is MUCH lower then of any 4th generation engine, which makes this engine more gasturbine, then a turbofan. So, judging by these facts i assume that F-119 allows supercruise without afterburner because it's afterburner was abolished in favor of main combustion chamber. Engine simply charges more fuel to the turbine, shifting combustion to the one point. Though it's not as simple as may seem - you'll need much stronger materials.
Hope this answers the question. If im correct ofcourse.
you just dissed F-22. This is going to be a truly stealth plane. It was designed to have < 0.1 m^2 RCS. I read a number 0.0027. Just for reference, the RCS of su-27/30 is probably 10 m^2.sumdud said:Hmmm..........
In an A2A battle, I'll take Aluka's words. It's relatively hard to detect a F22 w/ a ground radar since the plane's radar wave are going forward, and unless you are lucky enough to get the plane at an angle, your waves will simply deflect off the plane.
But in an A2A battle, the F-22's radar is on.(Note that the F-117 and B2 have no radars onboard.) And I am 99.999...999....% sure that the Raptor carries an active radar, you can detect the plane head on by receiving the Raptor's waves. And if you've noticed the back of the F-22, it isn't very stealthy, rather curved, meaning that if you are on its tail or on top of it, you can probably detect the plane conventionally.
It is disturbing to me that while the F-22 can achieve Supercruise(Flying faster than the speed of sound without the use of an afterburner), it can only achieve Mach 1.8, while the F-15 with a less powerful engine can do 2.5. But I guess I need some physics review here?
The manuverability of the Raptor is above average. It is better than that of some planes, but definitely behind that of the Flankers and Fulcrums. The Berkut, off course, I believe, has maybe the most mauverability w/o TVC. It and the MiG-35, Su-37/MKI definitely grabs top 3.
Yandex?
The Flankers and Fulcrums are in no way copies. Their engine intakes alone are unique.(The only fighter in service to feature dual, spacedivided under-intakes.) And as for the Frogfoot, anyone smart enough can think of the design!!!!!
I thought the MiG-1.42/1.44 was only a demostrator.
2D nozzles are fine with the roll rate of the Raptor.Although its 2-d, but that's still TVC.
Did you read info? Key characteristics are classified. And this is not an ass, you see the picture, and it does not have an afterburner on it. It's also not very clever just to say crap about others without any ideas of yours.Why bother with boring facts when one can speak right out one´s ass ???
By referring to division degree i refer to the parameter that is <air charge through outer circuit>/<air charge through first lowpressure stage>. Probably it's bypass ratio, i do not know western therminology. And if engine has an afterburner it does not make much difference, this parameter is still much lower, then of majority 4gen turbofans (judging by the picture once again).compressors division degree: seems you are refering to the bypass ratio, right?
According to P&W, F119 is an argumented turbofan
Afterburner is a second stage.Two stages of burners next to each other? I doubt so. That'll waste a lot of fuel.
Its combustion chamber. Air inlets are tiny holes in the chamber (you can't see them on picture), it's made to make more efficient diffusion between air and fuel.Wait then, what's that chamber in the middle of the engine then? Should've been the internal chamber of the turbofan, where the 1st burn is, but no inlets.
bd popeye said:I'm not sure how to react to this statement. I know you were not refereing to me. I always do my best to back up what I post. Thank you....