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wrightwing
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Posted: Mar 05, 2012 - 07:22 PM
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Elite 2K

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SpudmanWP wrote:
The F-22 cannot fire a 9xBlk2 in LOAL in HOBS mode due to it not having either a HMS or EODAS capability, although it may use off-board targeting.
Yet. That's what the MLD upgrade will provide though. |
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Posted: May 20, 2013 - 11:27 AM
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SpudmanWP
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Posted: Mar 05, 2012 - 07:39 PM
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Elite 3K

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If they have the money, yes it can be done.
Personally I think the MLD upgrades are more important than a HMD. |
_________________ "The early bird gets the worm but the second mouse gets the cheese."
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disconnectedradical
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Posted: Mar 05, 2012 - 11:37 PM
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aaam wrote:
popcorn wrote:
IMO if the AF wanted 3D TVC nozzles badly enough on the F-22, they would have found a way to do so. It's likely they didn't think the extra complexity and, more importantly, the less stealthy circular nozzle, was worth it. I understand that the rectangular nozzles on the Raptor engines result in.less thrust output, if true, a price they were willing to pay for superior LO. As far as maneuverability/agility, the F-22 does just fine from what we know
Don't forget, we're talking late '80s here. Do you think they wanted to pay what it would cost to invent it? Remember also, the YF-23 didn't use thrust vectoring at all and it also exceeded USAF's maneuverability requirement.
IIRC, the F-22 meets or exceeds the maneuverability requirement even without thrust vectoring. |
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aaam
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Posted: Mar 05, 2012 - 11:43 PM
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wrightwing wrote:
aaam wrote:
popcorn wrote:
IMO if the AF wanted 3D TVC nozzles badly enough on the F-22, they would have found a way to do so. It's likely they didn't think the extra complexity and, more importantly, the less stealthy circular nozzle, was worth it. I understand that the rectangular nozzles on the Raptor engines result in.less thrust output, if true, a price they were willing to pay for superior LO. As far as maneuverability/agility, the F-22 does just fine from what we know
Don't forget, we're talking late '80s here. Do you think they wanted to pay what it would cost to invent it? Remember also, the YF-23 didn't use thrust vectoring at all and it also exceeded USAF's maneuverability requirement.
There were a number of US aircraft that flew with 3D TVC, prior to the YF-22 ever being built, so it's nonsense to suggest that it was an engineering issue. Additionally, just like the F-117, B-2, YF-23, the F-22 was designed with IR signature reduction in mind. The only time you'll see flames coming out of the tail, is when afterburners are used, and then you're not really concerned about IR reduction. The F-23 had a plume when in afterburner as well. It was no afterthought to use cool air, to reduce exhaust temperatures, active cooling of the airframe/leading edges, IR signature reducing paints, and nozzles that reduce the size of the plume, from the frontal/side aspects.
As for NEZs, stealth reduces the effective range that the F-22 can be targeted, well below the missile's kinematic capabilities. Super cruise further reduces the window of opportunity. Having to shoot up at a higher flying F-22, further reduces the missile's effective reach. You have to remember, NEZs are dynamic, and situationally dependent. The aspect, speed, altitude all play a role in determining that range, along with the fighter and missile's abilities to detect/track/lock on to the F-22.
The two US aircraft I am most aware of that used 3D TVC were the F-15 ACTIVE and the X-31, both of which flew well after F-22 was designed, so their data wouldn't have been available for use in the F-22 design, which is why I said Lockheed would have to invent it themselves to get it on the YF-22. Regarding YF-22/23, of course Lockheed didn't ignore IR stealth, it's just that the YF-23 was more concerned about it. The nature of TVC means the exhaust has to be at the vary tail of the a/c, and 'burner or not, it's much harder to suppress the IR there than if you do it the way the YF-23 did. The flame is just a useful way of seeing this, and again, the point I was making was that you can only see the flame, 'burner or not, on the YF-23 is from a narrow cone in plane with the a/c. They were more concerned with that that Lockheed was, which is one of the reasons they didn't include thrust vectoring (interestingly enough the F-23 NATF did propose thrust vectoring and was an admittedly less stealthy bird than its AF counterpart).
You and I are not in disagreement regarding how the NEZ is dynamic. What I am trying to express is that while all the factors you mention in the post above are indeed valid, radar stealth is not a potent factor regarding the NEZ because if you can't get a lock, the NEZ (which is an aerodynamic thing) doesn't apply. |
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aaam
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Posted: Mar 05, 2012 - 11:48 PM
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wrightwing wrote:
SpudmanWP wrote:
The F-22 cannot fire a 9xBlk2 in LOAL in HOBS mode due to it not having either a HMS or EODAS capability, although it may use off-board targeting.
Yet. That's what the MLD upgrade will provide though.
But that's still years away. I'm not familiar how you can use offboard targeting to cue an AIM-9X's IR seeker unless another F-22 is using radar and then communicates to the launching F-22 where to point the -9Xs's seeker which then "sees" the target before launch or through LOAL once the Raptor is capable of doing so, but said seeker still has to achieve the lock sometime. |
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aaam
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Posted: Mar 05, 2012 - 11:57 PM
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wrightwing wrote:
aaam wrote:
I understood you were referring to getting in position to launch. What I'm getting at is that when the Raptor chooses to dogfight, it gives up many of the advantages that makes it what it is. It puts itself in an arena where it can be locked up by a weapon that will outmaneuver it.
The Raptor has proven very capable in WVR and BVR, so it's not giving up a lot. Obviously targets will be taken out at BVR first, but after all the AMRAAMs are expended, it will have to use the Sidewinder/Gun option, if there are more targets. Once the -9X Block II with LOAL is integrated, then the Raptor will be even deadlier in WVR, as it'll have all of its current advantages, plus similar capabilities to the F-35.
F-22 is unquestionably real good at WVR. When it comes close in, though, it gives up its altitude and speed advantages (which I think are as important as its stealth), it also gets into an aerodynamic contest that it could avoid (is Raptor really that much more agile close in than Typhoon or the latest Sukhois? --we're approaching the limits of effective human endurance here). Most importantly, it becomes vulnerable to that bugaboo that kills so many: while working one problem, you never see the guy that comes zooming in from left field, hoses off a shot and keeps going.
F-22 is no doubt the premier dogfighter, but it's even better when it doesn't. |
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shingen
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Posted: Mar 06, 2012 - 04:02 AM
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| I don't think the Raptor or Typhoon is going to get into WVR in any but extreme circumstances. They're both expensive and designed for BVR. The Typhoon uses the ASRAAM which is faster and longer ranged than other WVR missiles while the F-22 only carries the 9M for now. It would be interesting to read about a Raptor Typhoon, Raptor Sukhoi or Typhoon Sukhoi dogfight but it's not the way it's supposed to work. |
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wrightwing
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Posted: Mar 06, 2012 - 03:29 PM
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aaam wrote:
The two US aircraft I am most aware of that used 3D TVC were the F-15 ACTIVE and the X-31, both of which flew well after F-22 was designed, so their data wouldn't have been available for use in the F-22 design, which is why I said Lockheed would have to invent it themselves to get it on the YF-22.
There were quite a few design changes between the YF-22, and the production model. They could've included 3D TVC, if they felt that it was worth the effort. Signature management was considered more valuable, than whatever nominal benefits 3D TVC would provide.
Quote:
Regarding YF-22/23, of course Lockheed didn't ignore IR stealth, it's just that the YF-23 was more concerned about it. The nature of TVC means the exhaust has to be at the vary tail of the a/c, and 'burner or not, it's much harder to suppress the IR there than if you do it the way the YF-23 did. The flame is just a useful way of seeing this, and again, the point I was making was that you can only see the flame, 'burner or not, on the YF-23 is from a narrow cone in plane with the a/c. They were more concerned with that that Lockheed was, which is one of the reasons they didn't include thrust vectoring (interestingly enough the F-23 NATF did propose thrust vectoring and was an admittedly less stealthy bird than its AF counterpart).
Now you're changing your story. Both companies were given requirements, with regard to performance, signature management, etc...., and they both exceeded them. The fact that the YF-23 may have been better in certain areas, is irrelevant to whether LM paid any attention to that issue. There's more than one way to skin a cat, and LM chose a different way to do it. |
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tacf-x
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Posted: Mar 06, 2012 - 10:08 PM
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Both fighters exceeded the requirements for maneuverability, so at that point both contestants decided to mix in their interpretations on what the next gen should be like. I'm with aaam in that YF-23 used a far more novel and effective way to suppress IR emissions. It's use of heating tiles cooled by bleed air from the compressors is bound to be much more effective than Lockheed's idea. Not only that but I seem to recall seeing the engine nozzles for the YF-23 and noticing an extra nozzle flap above the ordinary nozzle flap. I believe someone on Secret Projects said it was used to manipulate the bypass flow of the engine to also aid in cooling the exhaust.
The raptor just doesn't seem to use such extensive means of hiding IR signatures. However the rectangular nozzles do help to shape the exhaust plume into a plume with more surface area per unit volumetric flow to make heat extraction easier. The two exhaust pedals should help in absorbing said heat from the flow. I'm not saying F-22's IR signature management is bad. I'm just saying it's nowhere near as good as YF-23 due to Northrop utilizing far more and far greater methods of management.
Okay, back on topic, 3-D thrust vectoring is overrated. I'm not exactly an expert (yet) but I seem to recall reading somewhere that the extra yaw performance and stability afforded by 3-D nozzles isn't worth the loss in IR and RF signature management. However I am curious as to how rectangular nozzles severely hurt thrust performance of the F-22?
Thrust is generally derived from evaluating the surface integral of the mass flows of air and their respective flow velocities at the ends of the engine. If you want high thrust you just need to ensure that there's a massive difference between the product of the exiting mass flow and exhaust velocity and the mass flow*initial velocity product at the engine face. At supersonic speeds you need a certain area ratio between exhaust area and throat area at a given back pressure and engine stagnation pressure to ensure optimum thrust efficiency.
What I'm wondering is how the shape of the cross-sectional areas at exit and throat could make such a difference for the F-22? Does anybody know or can provide a link for this? |
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wrightwing
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Posted: Mar 06, 2012 - 10:31 PM
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Elite 2K

Joined: Oct 23, 2008 - 04:22 PM
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aaam wrote:
wrightwing wrote:
SpudmanWP wrote:
The F-22 cannot fire a 9xBlk2 in LOAL in HOBS mode due to it not having either a HMS or EODAS capability, although it may use off-board targeting.
Yet. That's what the MLD upgrade will provide though.
But that's still years away. I'm not familiar how you can use offboard targeting to cue an AIM-9X's IR seeker unless another F-22 is using radar and then communicates to the launching F-22 where to point the -9Xs's seeker which then "sees" the target before launch or through LOAL once the Raptor is capable of doing so, but said seeker still has to achieve the lock sometime.
The AIM-9X Block II has a datalink, just like an AMRAAM. This is how third party targeting could be used. |
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aaam
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Posted: Mar 06, 2012 - 10:47 PM
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wrightwing wrote:
aaam wrote:
The two US aircraft I am most aware of that used 3D TVC were the F-15 ACTIVE and the X-31, both of which flew well after F-22 was designed, so their data wouldn't have been available for use in the F-22 design, which is why I said Lockheed would have to invent it themselves to get it on the YF-22.
There were quite a few design changes between the YF-22, and the production model. They could've included 3D TVC, if they felt that it was worth the effort. Signature management was considered more valuable, than whatever nominal benefits 3D TVC would provide.
Quote:
Regarding YF-22/23, of course Lockheed didn't ignore IR stealth, it's just that the YF-23 was more concerned about it. The nature of TVC means the exhaust has to be at the vary tail of the a/c, and 'burner or not, it's much harder to suppress the IR there than if you do it the way the YF-23 did. The flame is just a useful way of seeing this, and again, the point I was making was that you can only see the flame, 'burner or not, on the YF-23 is from a narrow cone in plane with the a/c. They were more concerned with that that Lockheed was, which is one of the reasons they didn't include thrust vectoring (interestingly enough the F-23 NATF did propose thrust vectoring and was an admittedly less stealthy bird than its AF counterpart).
Now you're changing your story. Both companies were given requirements, with regard to performance, signature management, etc...., and they both exceeded them. The fact that the YF-23 may have been better in certain areas, is irrelevant to whether LM paid any attention to that issue. There's more than one way to skin a cat, and LM chose a different way to do it.
2D vs. 3D: Most of the changes from the YF-22 to the F-22 were refinements of an already solid design. To go from a 2D to a 3D TVC system, though is a massive change involving the flight control system, the design of aft end, etc. At the time the F-22 was designed, there simply wasn't that much data available to draw from. X-31 started in the early '90s and F-15 ACTIVE didn't fly until the mid '90s so for Lockheed to successfully incorporate 3D TVC into their existing design would have been a very significant, quite expensive and potentially risky strategy, given the state of the art at the time. Could they have done it? Probably. Would AF have been willing to pay for that? Not likely.
Not changing my story at all. All I ever said was that, "I'm not convinced that the AF of those days put that high a priority on IR stealth in a fighter". Those would be reflected in whatever (still classified) requirements AF solicited. Northrop/MDD put a significant premium on them. Clearly, the Secretary of the Air Force had other things that were valued more highly. |
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aaam
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Posted: Mar 06, 2012 - 10:51 PM
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wrightwing wrote:
aaam wrote:
wrightwing wrote:
SpudmanWP wrote:
The F-22 cannot fire a 9xBlk2 in LOAL in HOBS mode due to it not having either a HMS or EODAS capability, although it may use off-board targeting.
Yet. That's what the MLD upgrade will provide though.
But that's still years away. I'm not familiar how you can use offboard targeting to cue an AIM-9X's IR seeker unless another F-22 is using radar and then communicates to the launching F-22 where to point the -9Xs's seeker which then "sees" the target before launch or through LOAL once the Raptor is capable of doing so, but said seeker still has to achieve the lock sometime.
The AIM-9X Block II has a datalink, just like an AMRAAM. This is how third party targeting could be used.
Given its range the initial setup at least will be working through the launch a/c's systems. This is fine if the other a/c in the loop is another F-22, but if it's not, for as far out as the eye can see the F-22 will not be able to engage in the necessary two-way datalink. |
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wrightwing
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Posted: Mar 07, 2012 - 04:31 PM
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aaam wrote:
Not changing my story at all. All I ever said was that, "I'm not convinced that the AF of those days put that high a priority on IR stealth in a fighter". Those would be reflected in whatever (still classified) requirements AF solicited. Northrop/MDD put a significant premium on them. Clearly, the Secretary of the Air Force had other things that were valued more highly.
If both aircraft have significant IR reduction, then I'm not sure how you can say that it was an afterthought by the USAF. It was a requirement though, or neither company would've spent the time/effort/money. |
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wrightwing
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Posted: Mar 07, 2012 - 04:34 PM
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aaam wrote:
2D vs. 3D: Most of the changes from the YF-22 to the F-22 were refinements of an already solid design. To go from a 2D to a 3D TVC system, though is a massive change involving the flight control system, the design of aft end, etc. At the time the F-22 was designed, there simply wasn't that much data available to draw from. X-31 started in the early '90s and F-15 ACTIVE didn't fly until the mid '90s so for Lockheed to successfully incorporate 3D TVC into their existing design would have been a very significant, quite expensive and potentially risky strategy, given the state of the art at the time. Could they have done it? Probably. Would AF have been willing to pay for that? Not likely.
Bottom line, signature management was the priority. It's easier to achieve with 2D, than 3D TVC. |
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popcorn
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Posted: Mar 08, 2012 - 02:43 AM
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| Offboard targeting coordinates may be available from other sources via Link 16… The Raptor can receive Link 16 transmissions after all. |
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