Alright
Sorry for a delayed answer. Ok, since you have posted the schematic from patent itself, I’ve merged it with Su-27 schematic from SK manual. Its as official/valid as it gets:
EDIT: Its also interesting to see T-50’s inlet area is curiously larger than Su-27s.
Are you sure the Pakfa windshield is that large? i believe the aircraft is even smaller.
Because the doctrine for an armored helo is to operate behind the enemy lines, the US Army expected to do it so in a occupied Europa.
Every plane is a disaster signature wise in AB, I don’t think anyone is denying that.
You should watch the video, at the frame in which the 22 is displaying that huge IR spot, the aircraft is not using AB.
“Actionjack” should watch the video as well.
You guys should understand that all that “supercruiser stealth” is a big fat myth, if you have a engine that has a 5000kgf output at dry, and other with a 5000kgf at AB, both engines will shine at the same bright in the IR specter at 5000kgf of thrust.
Actually, is probably the one at AB will shine less.
There are not interceptors in the west, and the last attempt, te F22 was a failure in that field.
You are aware that the Il-102 is a tonne lighter, empty? Two tonnes higher MTOW. And has two tonnes more thrust.
So… seems the designer did a good job all around. How did you do?
I must say i believed the aircraft had a empty weight of 13Tm, so i’m right?
The Ilyushin aircraft was based on a outdated concept, I mean, waste weight for a gunner and a tail gun? in the MANPADs age?
The t-50 bomb bays are very long relative with the AA-12, and wide enough to hold 3 missiles in each bay if the arragment is similar to the 22’s bay.
Anyway, these bays are meant to deal with larger payloads.
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All these “corruption” charts and reports are multinational holdings whining because their bribe was not good enough, come on…this is old bull$hit
I’m actually somewhat surprised that the PAK FA isn’t replacing the MiG-31. I mean, with Mach 1.5-1.7 supercruise and plenty of gas, I would’ve expected that the T-50 can take over the MiG-31’s role. Unless the VVS is really interested in having a platform faster than the Mach 2.35 PAK FA.
Launching a missile from mach 3 make it a totally different beast than launching at mach 1.5.
I believe this is quite important for the russian territorial defence, the range that a missile can gain from a plataform like the Mig31 outmatch every 5th generation airplane, the height and speed are incomparable.
Why didnt Warpac states adopt MiG-23 en masse and still relied on MiG-21 by 1990?
Probably, because there was a plenty stock of spare parts, and the Warssaw pact states were not large enough to justify the operation of the Mig23.
Would be awsome if russians could fit two very high bybass turbofans in such flying wing in such arragement.
I would love to see that think flying.
Ok, first, the delta wing is a well proven configuration, very solid, and for high mach speed it doesnt need very poweful engines.
We cant really know about aerodynamics, I must admit, but your small plane seems to have a shape too complicated for such small size, why must have the Fanker/Fulcrum layout for such small plane?, you will save weight stuffing both engines in the same structure, instead putting them on pods, the reason why the flanker has such design is because is more practical for such size, because structural issues for its huge lifting body…but your aircraft is lighter (or it must be).
I believe the best configuration for a very small 5th gen fighter is the Mirage one, a delta wing, single engine, a V shape tail and a radar blocker, no canards, nothing more that would add more weight, topspeed, i think your configuration will fail in the real world (over weight, structural issues, aerodynamics, etc..)
I believe the mig41 is actually a modernized version of the mig31 and there is a typo or a mistake about its new spped, which will be increased, probably to M3-3.3