It matters a great deal.
Only if your mission allows you to bug out. What makes you think any other assets would be able to sneak in any better? Its not hard to have a fingers 4 with the tail ender doing a sweep to turn their nose around the area.
Not much point defending a target if you can’t actually… defend the target. 🙂
The higher RCS aircraft will always be disadvantaged though, with regards to detection range.
That is only relevant if the detection range is close enough to matter.
For example, if the EF-T can detect the F-22 at 150nm, what does it matter if the F-22 can detect the EF-T at 200nm?
I’d agree with all of that bar one little bit.
Having effective fuselage lift at angles of attack below 25 deg (or so) can make or break a fighter in terms of sustained turn performance.
Post stall maneuvering is all nice and fine, and can be useful in some situations; however Boyd’s energy maneuverability theory still rules the dogfight, and from that going to AoAs above 25deg or so is a direct route to death.
go ahead. but in fighter and transport world we do not pretend that we can seperate “body-lift” from “wing-lift”.
so this whole point is a moot point.
now if you are willing to go in technical details and speculate on the specific aspects, I am all ears.
On your first sentence you are indeed correct, readings are normally taken on the wing-body basis.
But it is not a moot point. Having a fuselage that is effective at creating lift is very useful at increasing L/D in severe turns. Of course, you are well aware that lift created along and close to the aircraft centreline is the most efficient in terms of induced drag.
As for which approach is most effective (F-22, PAK-FA or J-20)… you’d probably need a windtunnel to find out.
I would think that with its superb avionics, electronic equipment and countermeasures suite combined with a higher degree of sensor fusion that the F-18E/F models may well make for a far superior long range strike and interdiction aircraft..
Bahahahahahaha
With how many drop tanks or A2A tankers supporting?
Another issue that will continue to surround all stealth designs is how long will current stealth designs offer invulnerability as air defenses adopt even larger and more powerful AESA radars. From the early days of AESA development, a key goal was to build a radar that can detect a very small object like a cruise missile at a distance great enough to target and shoot it down or a larger object like a fighter with a very low observable treatment.
Airborne detection of stealth aircraft may have already been accomplished in a series of tests done at Edwards AFB, Calif. in the second half of 2009. Those with insight into the research say Lockheed Martin’s CATbird avionics testbed –a 737 that carries the F-35 joint strike fighter’s entire avionics system — engaged a mixed force of F-22s and F-15s and was able to target the F-22s.
“The F-35 mission systems suite is the most sophisticated and powerful avionics package of any fighter in the world,” said Dan Crowley, Lockheed Martin executive vice president and F-35 program general manager at the time of the tests.
The F-22 fanbois were told some time ago that the “LPI” radar is a load of bull.
Better start hoping the DoD produce the greenbacks to fund IRST integration on the F-22.
With regards the bit in italics – quite presumptuous to presume the performance of competitors that Lockheed will know very little about. *Probably* not wrong, but nevertheless indicative of Lockheeds arrogant nature – talk the talk, but continually fail to walk the walk.
I’d love to see the source where anyone said that the F-22 would be cheaper than the F-15.
Perhaps you could do with reading the ATF requirements before entering a discussion centred around how the F-22 dismally fails to meet its requirements.
The ATF was supposed to have something like 3 times the MTBF of the F-15, something like 1/3rd of the support train requirements, combat turnaround time half that of the F-15, be more field repairable than the F-15, for any maintenance to be much easier to access and get done than the F-15 and therefore have an overall maintenance cost approx 35% less than the F-15.
Did Lockheed actually meet any of those requirements?
Feel free to provide examples of both, unless you honestly believe the USAF doesn’t know how much it has spent thus far.
LM: We can build the F-22 so it is cheaper to maintain than the F-15.
USAF: We’ll go with that.
DoD: Whoops.
This hasn’t been demonstrated to be the case, but feel free to grasp at straws.
I’ll just continue to go on historical evidence of LM promising the earth and delivering sh!t.
Oh, and the USAF being too stupid to realise they are getting taken for a ride.
LM and the USAF have disputed the GAO/JET findings though, as not being representative of reality.
Yeah…. in reality things are probably much worse! :dev2:
which is a disadvantage(especially at the merge, where you need to keep an eye on your foe, or incoming missiles).
Yes, that is true…
It would be such a disadvantage if you were not able to direct your missiles just by keeping an eye on your foe wouldn’t it? :diablo:
As a weapons system, this was true. The Flanker and Fulcrum were competitive aerodynamically, but their avionics/weapons lagged behind(I know you’ll bring up the Archer, but that didn’t offset the BVR advantages the Eagle had).
Given how **** poor even the AMRAAMs performed over Kosovo…. I think that BVR advantage is something of a myth.
If it ever kicked off over the Fulda gap, the Soviet doctrine of mainly WVR IR missiles appears a lot sounder than the US approach of BVR dominated loadouts.
I was wondering how long it would be before the Russian fanboys start to try and take credit for the J20. :rolleyes:
:confused:
If you think there was no data cross over from TsAGI to the Chinese at the gestation stage of the J-20 program your nuts!
Again, that DOES NOT MEAN IT IS A COPY!
My point is that there are currently production representative F-35s flying, and double digit airframes available for testing, and we’re still looking at 5-8yrs till IOC.
Yeah… ‘cos the US way of going about it is the only way. :rolleyes:
and onto those who said it is Mig 1.44 stealthrized. vs Flankerism of PAKFA:
IT IS NOT MIG 1.44 Stealthrized.the chief aerodynamicist, spelled out his entire ideas for this thing in a paper published in 90s.(?), (with quotes to Bill Sweetman to boot. ). this is not a Mig 1.44. reborn.
Do you have a link, or even the title of the paper?
Anyway; to me at least, the similarities to the MiG 1.44 are too close to be totally unconnected IMO. Perhaps it was a starting point for the aerodynamic platform. Whether that came from the same research data from TsAGI that fed into the 1.44 program or whether it came from the 1.44 program directly I don’t know, but I certainly feel it has influenced the J-20.
[BTW that does not mean its a “copy”, only idiots would suggest its a cut and dried copy without sh!tloads of work to adapt the concept :)]