I guess the combat radius of Tu-22M3 with 2 kh-22 is around 2000 km, with mixed military and afterburner on the weapons deployment phase.
The problem of the Tu-22M3 is not range or speed, but obtain target information from the Tu-142 which will certainly get hit by CBG before passing any information to the Tu-22M3. And, the Kh-22 is not that impressive weapon. I have a link that talked about the disadvantage of high velocity, high projectile weapons such as the kh-22. Surface heating on the sensors of Kh-22 during high speed is one of its problem.
the Kh-22 is an impressive weapon. It is not without its problems, but if you think for a minute what it does, it is pretty impressive!
Haven’t seen the video yet, but i don’t think this can fly well.
oh it probably flies. well, is a different issue.
Well based on my very limited knowledge of aerodynamics, it would be fairly incapable of “High Alpha” flight. The intakes would be soooo blanked off by the fuselage there is no way they could gulp enough air.
I wouldn’t worry too much. This does not appear to be real. A propaganda vehicle maybe. But I don’t believe this is more than a mock up and not even a serious one at that.
…
As for the auxiliary intakes, try to guess why the wire grilles on the F-117 were sized the way they were ;).
The 23 was not chosen. People say it had better LO characteristics but we will indeed never know. Since it was beaten in the competition, we have to go by what the winner of the competition sports.
I am not talking about the sec. intakes themselves. I am talking about the discontinuities they introduce to the surface.
However general consensus is right, you cannot just assume how affects RCS by using eyeball. With appropirate continuity (which PAK-FA has by using very large composite panels) and correct RAM application (which PAK FA will certainly have in serial version) it may virtually be non-existant.
I am more concerned with returns from gaps, seams and discontinuities which the T-50 seems to be having aplenty.
Starting with the leading edge slats, the various vents and the gaps between the weapon bays. Especially the leading edge slats were a big puzzle to me. Both US fighters, the 22 and the 35 have a leading edge slat that runs all the way to the edge of the wing without leaving that characteristic dog tooth at the wing’s edge. The T-50 does not.
The devil is in the details.
Well it seems I have found something of high interest in the aviation world. Also I haven’t had much criticism of my plane design :D, yet. I agree in that a few ‘pre-programmed’ wing positions could be used (like flap settings), but some sort of computer would probably have to be used to make minor adjustments. Once again thanks for all your help, time to start a model I think!
The Wright brother’s flyer used adaptive wings. Just like a bird. The quest for this superior wing, started at the very beginning.
NASA i believe tested it on an F-18.
Why has nobody suggested Fatass?
Fatass would be cruel and unjust considering it has the slimmest profile of all the 5th gen fighters.
This is one of my concept aircraft I have recently designed and drawn. I would like to know if it could work as a real aircraft :confused:, any comments. A few points with this aircraft are:
Wing Design, loosely based on that of the Valkyrie (folding wing tips) and the TSR2.
Tail Plane, when moved, it re-directs the jet exhaust massively increasing effectiveness.
Four Jets, mounted onto the side of the fuselage (this allows space for landing gear and fuel in fuselage) I am yet to decide on what sort of engine to use, any ideas?Any comments will be much appreciated. 😀
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landing gear is too narrow. Engine wash affecting the tailplane is fine, but not when it is only from two out of the four engines. it would be ok if the engines were widely separated but not they are too closely coupled.
All military aircraft are weapons of war.
Their primary reason of existence is to kill.
Do not therefore be surprised that any military plane can achieve a kill against another. It is what they were meant to do.
I agree, though it’s more like a lower 1/3 (at worst).
Not necessarily, the circular frame of the ‘IGV’ is totally at odds with the engine alignment but that is not relevant. It’s the vanes’ positioning that do the work of ‘straightening out & directing‘ the airflow to the unconventional lie of the compressor.
You’d be absolutely right, look @ where the core nozzle is pointing (ignore the TVC nozzle petals):
Hence, the engine is directly aligned with the top cowling, and angled within the lower.
That would depend entirely on the material composition of the IGV (and the compressor for that matter), would it not? 😉
I beg to differ, I think you’ll find that infamous high-res shot has much more in common with the IGV (notwithstanding it’s in the same location). The engine cannot be substantially longer and have two bends in it.
Thanks man, appreciated.
Me thinks it worthy of reposting this here, to finally lay an old fallacy (and favourite whipping boy) to rest.
I think this is interesting. Perhaps you can help me with something.
1. The patent documents (that we have seen in this forum in .pdf) show the lower half of what looks like a compressor. The image doesn’t resemble that of a typical IGV.
2. Following from that, wouldn’t a typical IGV be aligned with the engine? Would there be an offset between them as is implied here? Wouldn’t that be counter intuitive for an IGV?
3. Although the upper half of the T-50 does indeed seem to indicate the engine must be pointing inwards somewhere behind the cockpit, the lower half clearly contradicts that with the nacelles pointing straight and the intake walls partially curving but NOT obstructing view to the engine.
4. Wouldn’t an IGV be another contributor to RCS in the duct similar to a compressor fan? perhaps not as much, must still.
5. The now infamous photo of the T-50 with the straight through duct showing the lower half of the compressor, in that photo it looks like a proper compressor, not an IGV, but it seems to be in roughly the same position. (some say that photo was ps’d I hear. )
any thoughts ?
If you read the next sentence (after the 72:0 comment), it seems that they are talking about the USAF.
I wouldn’t want to repeat the same thing that has been said many times over.
It is however true that in all the recent wars, there was no real credible threat to the USAF-USN.
If one was to take things into perspective, there is no western air force that could pose a credible threat to USAF-USN.
Just going to point out something:
panyimao and Tigershark are not the only problem. They are only 50 % of them problem. Other 50 % are all of you that answer or refer to them and therefor contribute with pollution of this thread and the forum.
Ignore them.
Can’t believe people are much more interested in discussing these two tards instead of staying on topic.
I won’t directly disagree with you, however if you never pay attention to negative comments, then you may end up with a forum that everybody su**s eachothers’ d*ck and no one ever pinpoints inaccuracies or has a meaningful conversation/debate.
And this statement highlights the misconception about F-35. F-35 is not about dominance in the air. F-35 is about finding and destroying highly mobile ground targets which are using sophisticated CCD techniques. This capability was found to be woefully lacking in Bosnia, Kosovo and Iraq. The premise is if you can kill mobile CCD targets, then killing any other type of ground target is easy.
F-35’s combat radius is far short of USAF and USN desires. USAF has initiated a Long Range Strike/Family of Systems program to address F-35’s range/capability shortcomings, but LRS will not see daylight until probably 2020-2025. And LRS is a family of vehicles, not a single bomber platform. http://www.dodbuzz.com/2012/07/25/csaf-long-range-strike-is-coming-in-the-20s/
Of course, this is my opinion written from a US long-term capability-centric needs perspective and ignores other nation’s platform-centric desires. (If you think F-35’s capabilities are too expensive for NATO members, then LRS is an order of magnitude worse).
I believe this is where a lot of criticism is coming from.
The majority of NATO air forces do not have dedicated air-superiority aircraft.
If one needs to acquire F-35’s one needs to be able to use them for air-superiority as well.
This is when the price/number/capability discussion begins.
Nope. How can i forget our F-16C Fleet.
It not the same for a Nation like Norway to operate F-16C in all different roles, and that includes Intercept mission as well.But that does not turn our F-16c into an Interceptors, does it?
You have jets like true Interceptors and then you have jets flying that role.
Not the same thing.
We agree, it is just that you stated it so absolutely and I wanted to point out that is isn’t so absolute as it came out to be.