The original count of spikes was 1,676, but that is completely wrong, as we already know. The number of valleys is ~1,624 (too lazy to count)..
Now, according to the drawing, last two valleys on each edge don’t have their own TRM. That means four valleys in each row. The row count is 52 lines = 208 TRMs less. 1,624 – 208 = 1,416 TRMs. Plus minus a few, give or take..The 1-to-1 arrangement doesn’t look similar to what we can observe on the APG-81 picture, I believe there will be APG-81(V)2 one day with higher TRM count, different arrangement and increased output power. But we’re not there yet.
The half spike in each line wasn’t counted in the first place
according to the pattern each line have 2 spike that isn’t TRM
so 52× 2= 104 TRM less
1676-104 = 1572
Btw neither of the pattern actually look exactly like F-35 TRM, so we only speculate here ( keep in mind that APG-81 use the latest gen TRM at the moment )
Yes, we have and based on the patent drawing you have provided the “valleys” on the edges don’t have their own TRM. The 1600+ number is not correct.
the pattern i posted shown that the outer “spike” may not have their own TRM, the original count of ” spike” was 1676, after minus 2-3 “valleys” on the edge of each line the number gone down to 1626, SpudmanWP also posted pattern shown that new TRM can be installed in a 1-for-1 arrangement.
http://forum.keypublishing.com/showthread.php?135460-test-pilot-quot-F-35-can-t-dogfight-quot/page22
I have no doubt that the APG-81 can be used as a jammer.
On the other hand it is X-band only and limited to 60-deg. off the nose.
one small mistake there
APG-81 angular coverage is actually 120 degree ( 60 degree left and 60 degree right)
While X-band is used for some SAM tracking radars, there is a growing number of lower-band radars that can direct a missile into seeker range. For instance, the Sea Ceptor (CAMM) is intended to operate directly with the E/F-band Artisan.
still the majority radar of fighter, AWACS, Ship, SAM are X band
and APG-81 isn’t the only jammer that F-35 carry, it can also transmitt jamming signal through ALE-70 ( similar to the way F-18 E/F use ALE-55) , there are also MALD-J, and in future F-35 can integrate NGJ as well.
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Also, in order to perform continuous jamming, the “stand-off” jammer has to keep the target inside the arc of coverage, which means that it is closing the range to the target.
You can have 2 fighters taking turn jamming enemy’s radar
There is no mention about the EA capabilities of the APG-81, whatsoever. And even less is there a mention about hi-power EA jamming
that wrong
. All three variants of the F-35 carry active, electronically scanned array (AESA) radars with sophisticated electronic attack capabilities, including false targets, network attack, advanced jamming and algorithm-packed data streams. This system allows the F-35 to reach well-defended targets and suppress enemy radars that threaten the F-35.
While F-35 is capable of stand-off jamming for other aircraft — providing 10 times the effective radiated power of any legacy fighter — F-35s can also operate in closer proximity to the threat (‘stand-in’) to provide jamming power many multiples that of any legacy fighter.
https://www.f35.com/about/capabilities/electronicwarfare
. The APG-81 has some ~1,450 TRMs,
actually 1626 TRM, we already discussed this
rated 10-12W each, the total power output is some 14-16kW, what high power are we talking about, at all? The old ALQ-99 has almost 11kW dedicated to jamming alone. Is that the device intended to fry enemy radars at dozens of kilometers? Don’t be silly. The article doesn’t mention anything of the sort.There is no high gain EA with the F-35. There is simply EA, surely quite advanced once developed complete. But the idea of the F-35s flying around and using its 15kW power to cancel all radars in the vicinity while staying completely unaffected by megawatt-class ground-based radars doing the same, do you realize how dumb that sounds?
ALQ-99 use normal antenna thus it transmitted jamming signal in a very wide cone ( basically like a low gain radar) , the advantage is wide coverage, the disadvantage is that power isnt focused, thus the signal to noise ratio is high at the enemy’s radar location, by contrast AESA can focused it’s beam into a very narrow cone, as a result with similar out put an AESA jammer will be significantly more powerful than a legacy jammer
Lower RCS does reduce detection range alone, it also reduce burn through distance , and jamming power required will decrease in the same rate as RCS reduction ,50% reduction in RCS = 50% less power required to overwhelm real radar reflection with noise ( you can work it out for yourself , 99.9% reduction in RCS= 99.9% less power required to achieve same level of effectiveness , and so on )
now let take example of 4 aircraft :
1) B-52 : RCS = 100 m2
2) EA-18G : RCS = 10 m2
3) Mig-35 : RCS = 1 m2
4) F-35 : RCS = 0.001 m2
now compared them :
from B-52 to F-35 then RCS is reduced by 99.999% =>99.999% less power require
from EA-18G to F-35 then RCS is reduced by 99.99%=>99.99% less power require
from Mig-35 to F-35 then RCS is reduced by 99.9% =>99.9% less power require
( if you not good at math then use this http://www.percentagecalculator.net/ the lowest row )
so again a very powerful enemy radar : if F-35 need 5 kW jammer to shield it’s radar reflection with noise signals then Mig-35 will need a 5 MW jammer , EA-18G will need 50 MW jammer , B-52 will required 500 MW jammer , you can argue that bigger aircraft can carry more powerful jammer but remember even the SPY-1 only have power of 5 MW.
My point? , If EA-18G can protect itseft from SAM by it’s jammer then a VLO can also do that, and actually it will be alot easier for them
What an humorous ability.
I place currency on wager that users of F-35 will make sure of integration of EW pods and specified wingtip jammers.
You do know that the only reason this ability of APG-81 exist only to provide a jamming capability because to place external jammers would ruin all the painstaking effort to improve by 95% over 4th generation aircraft?
If you wish to verify,
[ATTACH=CONFIG]239407[/ATTACH]It become obvious to say that this ability is very unuseful, as it turns the jammer to a very high probability of destruction beacon.
This radar mode is only useful against third world nations with no IADS worth speaking of, where passive sensors simply do not exist.
F-35 can also carry ALE-70 ( work in similar fashion with ALE-55), so it can jam by that as well, the advantage of AESA jamming is that it can focus power into a narrow beam, thus achieved high ratio noise to signal at target place
While F-35 is capable of stand-off jamming for other aircraft — providing 10 times the effective radiated power of any legacy fighter
https://www.f35.com/about/capabilities/electronicwarfareIt’s low RCS also benefit jamming
http://www.rfcafe.com/references/electrical/ew-radar-handbook/radar-cross-section.htm
and it have been explained like a thousands times RWR cant really provide firing solutions again moving airborne target
There are also other F-18 pilots that are not entirely convinced in that story
I do heard F-16 pilot said F-22 and F-35 canopy doesn’t offer as much vision as their bubble shape canopy, …. etc but i haven’t heard F-18 pilot complaint about F-35 high AoA capabilities
high F-35 officials that claim that the plane is not as capable as legacy fighters in some scenarios.
You mean less agile? , because i dont see how F-35 can be less capable
Here is the video of F-18 HARV doing 180° loaded rolls at different AoA`s, going from 5° to 35°.
https://www.youtube.com/watch?v=SViiqylV0lA
Here is the video of Su-35S at 2:56 sec. doing 360° roll close to 70° AoA.
https://www.youtube.com/watch?v=XyrM3VHst1k
Here is another video of the same maneuver at 3:53 sec. but from another perspective.
https://www.youtube.com/watch?v=rPzBaQnkDTk
If you measure the time you will see that Su-35S is doing the roll about two times faster at almost two times higher AoA. There is video explanation of the similar roll manuver Su-30MKI is performing where they claim 70° AoA, but I can`t find it now.
The height and the speed for both planes (Su-35S and F-18) are not identical but it is not hard to see the difference in performance at such extreme conditions
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the su-27 in video look like it doing a scissor maneuver rather than a roll
nevertheless i dont think you can look at these video and concluded that Su-35s can roll 2 times faster than F-18 at 2 times AoA because you simply dont know their fuel load ( it is liklely that aircraft in air show doesn’t carry full fuel tank) , you dont know their respective altitude ( it look like the F-18 is at higher altitude and aircraft maneuver ability reduced as altitude go up) , you know the speed of F-18 but dont know the speed of the Su-35s….etc
Not everything. The planes such as PAK FA or Su-35S can have extremely fast pitch and yaw rates and ridiculously small turn radius at such conditions that are not possible for other planes no mater at what flight conditions they are (slow-fast, low-high). In other words, it is very important to have such capability when you and your opponent are going slow (superior nose pointing)
Su-35 and PAK-FA can have very good high AoA and nose pointing capabilities because of their TVC, however even them are at very low energy state ( very low speed, partly stalling) when they perform such maneuver
and the pilot can also trade the speed for the first shot if he finds that to be suitable in the moment.
yes when pilot turn faster than his max sustain turn rate he basically trade speed and altitude for nose pointing ability
And in the days of modern SRAAM`s the winner is usually the one that can lock and fire first.
agree
WHAAT? Mig-31 doesn’t get really new features when compared with Foxbat?
Turbofans instead of turbojets
well, with tuborjet engine Mig-25 will have better performance than Mig-31 at very high altitude
, two seater,
well there is also a version of Mig-25 with 2 seat
4 long range missiles with TVM (track via missile, given your last exploit better to write it in full words),
R-33 is SARH
R-37 is ARH + mid course guide + SARH
i dont think either of them have TVM capability
TVM would required 2 way datalink
first airborne PESA radar…
F-16E changed to AESA radar, and it’s performance isnt much difference from F-16C/D
And you even use it as your nickname…
what i mean is, there isn’t that much significant change between Mig-25 and Mig-31 compared to F-16 vs F-35
New radar? : well most fighter have new radar in every block upgraded
New engine? : it quite common that fighter have new engine in their upgraded block
New weapon? : quite similar to these above
Mig-31Bm, you have made a gigantic error there. ARH is Active Radar Homing, not Anti Radiation Missile (ARM)…:o
AIM-53, AIM-120, Standard 6, Meteor, AA-12 Arrow, S-400 missiles…
LoL, my bad, i reply too fast, and some how i thought that ARH = anti radar homing 😀
TSFC 1.92? compared to what?
TSFC = thrust specific fuel consumption which can be expressed as lbs of fuel burned per hour for every lb of thrust., so i dont really understand what you mean by ” compare to what”
Altitude? Thrust and fuel used is dependent on the amplification ratio. The stoichiometric ratio remains the same, so it has to adjust on the altitude gained.
i was considered dogfight situation so aircraft are going to fly at relative similar altitude, and they aren’t going to fly very high in dogfight either ( due to thin air at high altitude, sustained G is not very high, aircraft will turn very badly at high altitude, if they make high G turn they will lose speed and altitude very quickly)
Speed. What is the ram-recovery of the intake and the thermal efficiency of the engine?
Irrelevant here, Fixed intake work well at least until mach 1.4, pilot arent going to accelerate past mach 1 in dogfight
6.9 minutes reheat? Is the reheat system cleared for that length of time? Is it a 1750K or 1900K system? what damage can occur when the heat has stretched the reheat pipe?
prolongued AB isnt being such an issue for engines in 80s and onwards. Supposedly only earlier engines suffered that limit. That doesn’t mean new engine itself would last as long if it was on full AB all the time, sortie after sortie. But that within a single sortie the pilot could afford to use as much AB he deems necessary without fear of engine dying out on him right there during that sortie
Gasflow. Are you talking about sonic or supersonic gasflow through the engine?
if the air go through engine at supersonic speed the engine wont work, the reason for variable intake, Ram.. etc is to reduced speed of air to subsonic before it go through the engine
I think your time on afterburner calculation is meaningless in real world conditions unless you want to burn all your fuel at sea level conditions.
For example, given that air density represents the mass per unit volume of air, a jet engine will produce far less thrust at high altitude where the air is less dense, and since we know that fuel flow is directly related to thrust (it is thus thrust-specific) and that for example, in supersonic cruise conditions thrust equals drag (and there is so much less drag at high altitude), the plane can go very fast for longer time with far less thrust using less fuel compared to sea level conditions.
You can`t just use the sea level static thrust numbers for engine max power and thrust specific fuel consumption number to calculate for example the range and time on burner at higher altitude without knowing the engine thrust numbers at that specific height and drag of the plane at given speed and height. The performance figures for two different planes, such as Su-27 and F-35 will be different even if they have the same time on afterburner at similar conditions. One can for example travel at Mach 2 speed and the other can travel at Mach 1,6 for that period of time. That would be a huge difference in performance.
Also, TSFC is not constant, it varies (probably not that much) with altitude, flight Mach number, ambient temperature, throttle setting etc.
Yes i do aware that TSFC isn’t a constant value, in fact if you read several pages ago, i was the one correct MSphere on that,
TSFC go up as speed go up and go down as altitude go up,
my calculations was only meant to show the time on afterburner of these aircraft relative to the other in a given conditions, in dogfight, aircrafts are likely to fly at around the same speed around mach 0.7-0.8, ( no one will accelerate to mach1.6 or mach 2 in dogfight) and fly at same altitude, thus the effect of air density will affected them in quite similar fashion, as a result their respective ratio of times on afterburner will be quite similar.
For example : my calculations shown F-15 on internal fuel can have maximum 6.9 min at full afterburner at sea level, F-35 have about 13 minutes, in reality the time of both will be more or less depending on the altitude they fighting, but the F-15 on internal fuel wont have more time on afterburner than F-35, that the point
When we talk about maneuverability/agility it is also very important to be very specific about number figures and almost every information about F-35 is not that specific. For example, they say it has ability to exit at 50° AoA in controlled fashion and it seems that this is enough to assume that it has F-18 high AoA nose pointing ability?
I don`t think so because we don`t know about its pitch, roll/yaw rates at that conditions. I`m not saying it is inferior than F-18, I really don`t know, but other than 50° AoA there is not much useful information. F-18 is rare plane that can comfortably roll at high AoA and can point its nose in every direction,
according to test pilot F-35 have the high AoA characteristics of F-18, that all we know, it is very unlikely that we can get F-35 EM graph any point in near future ( same for all 4.5 and 5 gen fighter) , so the best we can do now is make educated guess.
btw here is the only video of F-35 in post stall, high AoA test that i can find
http://theaviationist.com/2013/05/21/f-35-aoa-test/
but for the time it can finish 180° roll at 35° AoA, Su-35S can finish 360° roll at almost two times higher AoA. In other words, both planes can roll at 35° AoA but the difference in roll rate will be significant.
i dont think Su-35S at 70 degree AoA can roll 2 times faster than F-18 at 35 degree AoA
And if the F-35 is sluggish at high angle of attack conditions, than its ability to exit 50° AoA is not of much use.
well, everything are more sluggish in high AoA due to high drag, they are not going to fly as fast or turn as fast as they normally do at low AoA
mkellytx has supplied valuable insights regd. the reasons and conditions the test has taken place. For that I am grateful..
But neither he nor your charts can debunk a rather simple summary written in the original report..Overall, the most noticeable characteristic of the F-35A in a visual engagement was its lack of energy maneuverability
you forgot to read this
Irrelevant of F-16’s qualities, the statment above explains WHY this cannot be a dogfight and all comments about F-35’s sustained performance is nonsense; in simplest terms high AOA maneuvers and energy maneuverability is mutually exclusive.
and this
Well, technically you’re still EM, just on the left side of the chart out of E b/c you didn’t M. Your point however is taken that the F-35 wasn’t taking an EM approach. As we both agree the test wasn’t about managing energy it was about getting the nose high and seeing if you could make it do the funky chicken when you slam the controls around trying not to hear, “Guns, guns, guns”.
btw f-16 pilot seem to think even the F-15 and Su-27 are not good at retain energy in BFM compared to F-16
look all im not saying the f-15 isnt amazing, I’m just saying that even F-15 pilots will admit that the viper is a better BFM machine when flown properly. We can hold our energy waaaay longer. The f-15 is much like an F-18 in that it has High AOA ability and can really yank the nose around once. Then it is a pig in space with no energy and is easily killed. Vipers practice BFM with a centerline tank and catm missles. The only drag increase in actual combat would be the addition of a sniper/lighting pod.
no, because F-35 didn’t have anything going for it performance wise compared to the old underpowered F-16D with two tanks
wasn’t an actual pilot explained this like 20 pages ago
http://forum.keypublishing.com/showthread.php?135460-test-pilot-quot-F-35-can-t-dogfight-quot/page9
…
I was much more modest thinking you was referring just to the ones like speed, climb rate and acceleration that were related to a scramble mission.
So according to your own word I was totally right when I said that F-35 specialized into being a flying brick.
Man, and I though I was just joking (or better saying a sad truth with an half smile):rolleyes:.
Comparable to bomb loaded F-15E and F-16, you mean.
Still have not noticed that all those fancy brochures refers to A2G loads???
And F-15E is not used for air defense roles anyway, C&D without conformal tanks are
It feel like you just skip everything positive about F-35 that have been said so far in this thread, it have already been stated that F-35 have quite compatible turn rate with F-15 and F-16, it’s AoA capabilities is around the same as F-18 and it’s acceleration rate is similar to su-27.
Lets all fueled to fly 500 nm distance and back
F-15E need 58% fuel, total weight = 18000kg
F-16C need 83% fuel. total weight = 11735kg
F-35A need 57% fuel. total weight = 18082kg
Su-27 need 40% fuel. total weight = 20060kg (40% should make 500nm return trip)
While all can pull 9Gs, their ITR will differ by speed;
F-15E = 17,17 deg/s @ 292 m/s,
F-16C = 16,07 deg/s @ 313 m/s,
F-35A = 17,6 deg/s @ 285 m/s,
Su-27 = 20,96 deg/s @ 240 m/s
Now that is about max turn rate, how about time on afterburner :
Let start with su-27
TSFC of AL-31 is 1.92 at full AB
thrust at full afterburner of AL-31 is 27560 lbs
Su-27 have 2 engines so it will consume 105830 lbs/hours
Su-27 internal fuel capacity is 20725 lbs so with full internal fuel it have around 11.75 minutes on full afterburner ( with 40% fuel, it will last 4.7 minutes)
F-16C/D ( no CFT)
TSFC of F-110 GE129 is 1.9 at full FB
thrust at full afterburner is 29500 lbs
F-16 have 1 engine so it will consume 56050 lbs/hours
F-16 internal fuel capacity is 6972 lbs so with full internal fuel it have around 7.5 minutes on full afterburner ( with 83% fuel it last maximum 6.225 minutes on full afterburner)
F-15C ( no CFT)
TSFC of F-100 PW229 is 1.94 at full AB
thrust at full afterburner is 29160 lbs
F-15C have 2 engines so it will consume 113140 lbs/hours
F-15 internal fuel capacity is 13123 lbs so with full internal fuel, it have about 6.9 minutes on full afterburner ( with 58% fuel it last maximum 4 minutes on full afterburner )
F-35A
TSFC of F-135 is said to be 2 at full AB
thrust at at full afterburner is 43000 lbs
F-35 have 1 engine so it will consume 86000 lbs/hours
F-35 internal fuel capacity is 18498 lbs so with full internal fuel it will have about 13 minutes on full afterburner ( with 57% fuel it last 7.41 minutes on full after burner)
For what I know both F-22 and (in future) PAK-FA sacrificed very little compared with, respectively, F-15 and Su-27/30 i.e. their antecessors and I think it was more because of stealth added features.
F-22 is extremely expensive
PAK-FA sacrifice part of stealth capabilities to get more kinematics
MiG-31 also when compared with MiG-25 doesn’t sacrificed anything substantial in key performances.
because it doesn’t really get new feature ( F-35’s feature different from F-35 are : ability to fly very far on internal fuel , VLO characteristics, internal weapon bays
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Sorry, I was under the impression that strike fighters, VLO or not were done to penetrate enemy air defenses, avoid enemy interception and SAM, attack targets and possibly come back
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i dont think you understand what i mean
what i said is : if FCR can detect and track VLO platform as easy as normal platform then no one would bother spending money on stealth aircraft, they will just make normal fighter
About SAM missiles allow me to spend some words more:I had said on purpose modern, last generation SAM meaning with this the ones with ARH guidance.
anti radiation seeker is impractical for an AAM, or SAM because they will be useless the moment enemy aircraft turn their nose away or turn off their radar
the only thing you can hope to shot down by an ARH AAM or SAM is an AWACS than constantly transmissting and moving in the same direction the whole time
Low band radars doesn’t gave a precise positioning of a target but they were in the old times coupled with targeting radars but actually they are perfectly capable to get enough precise data to perform mid course guidance for ARH missiles in order to put them close enough to lock on target on their own.
It is not easy, it is expensive in terms of upgrading cost but just a fraction of what it is necessary for get VLO planes.
low band radar isnt accurate enough even for mid course guide, even something as new as the NEBO VSU have elevation error of 3-5 km
Flying at 60kt and at any speed is obviously a suicide WITHOUT ECM, ARM, heavy jammers suites and so on.
Now the point about metric wavelenght radars is that it is actually a suicide also for stealth airplanes, above all if they were designed to operate for long period at those quotes deep into enemy territory or without such systems on board….
flying at 60K ft, your aircraft sustain turning capability will be around 1.5-2 G, basically supper sluggish
and as i explained before metric wavelength radar isnt accurate enough for weapon guide, they are also huge, stationery radar that make perfect target for cruise missile ( jassm, jsow, tomahawk, jsm.. etc)
FYI : F-35 can jam enemy’s radar by it’s APG-81 ( because it have very low RCS the jamming power required is significantly lower than legacy fighter ) ,
F-35 can also carry FOTD : ALE-70
Well, since most of theis is classified it has to be. But just going on facts instead of how jamming and radar works we can look at history yet again.
From Allied Force:
It was only carried on US F16 and being the jet flying most dangerous missions (low and medium alt daytime) + following the F117 on all nightly raids.The F16s had a sortie rate of well over 2:1 compared to the F117 and only half as many hit aircraft. Surely not all of this can be attributed to the AN/ALE-50, but according to pilots it had a huge impact on survivability.
In the end the F16 had a ratio of missile evasion of just above 4:1 compared to the F117 on a sortie by sortie rate.
F-16 didn’t fly the most dangerous mission, F-117 does, at least according to USAF
also ALE-50 was used again relatively old SAM system
Coincidentally pretty close to the succesrate I attributed to the far more superior BriteCloud when fired in swarms of 3.
Most AAM also have ECCM capabilities themselves so the effectiveness of BriteCloud again Meteor, AIM-120D is also questionable, Even if we discount the ECCM ability of AAM, they can still be supported by the launching aircraft through data link and it is alot harder to jam the aircraft radar compared to a missiles especially if that aircraft have AESA radar ( i dont think Britecloud can do that)
AAM will also have AESA radar seeker in future making it even harder to jam them ( from what i know, Russian already making prototype of AESA seeker for R-77, Japan cooperate with MBDA to make a new version of Meteor with AESA seeker for their F-35)
And there is nothing say that future long range AAM cant have IIR seeker, we already have a few of them like MICA IR, NCADE, R-27 IR… etc, Israel also have a programme to convert their Sturner SAM to AAM, stuner have both EO and RF sensor.
P/s : i think most on battlefield most soldiers would prefer to have a gun than a bullet proof vest and a knife
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Now who is pulling numbers from their a$$? You can expect radar detection range, in real life, to be from roughly 0-200km in a jammed environment. The lower end is less likely but was demonstrated by Su30MKIs vs F15C.
F-15 in these exercises only have MC radar, thus they are alot more vulnerable to jamming compared to AESA radar
Most common method used to decoy missiles, enemy radar is deceptive jamming (or DRFM) which have been used widely on many jammer such as ALQ-211, ALQ-184, ALQ-214. Some people (I.e. Kopp and Goon) see as the end-all in air-air warfare. However, repeater jamming depends on picking up the radar emissions of the missile/aircraft – if the ESM doesn’t detect the radar and recognize it (such as if the radar is AESA LPI set, APG-79, APG-80, APG-81.. etc ), it doesn’t have any signal to repeat back to the receiver, and so it can’t create false targets.
For DRFM to work, it has to detect a signal (radar pulse or pulses) to memorize and to generate the false targets. LPI radar on the other hand tries to hide the real radar signal in noise to counter that. The problem for jammer is that it doesn’t know what kind of signal the radar is sending (mismatched filtering), but the radar of course does (matched filtering). This is not a problem with relatively simple radars as the signals they send are also simple and do not change. So once the signal is detected, it can be stored and easily used against the radar.
Modern LPI radar on the other hand does a lot of things to make things very difficult for EW systems. They send complex waveforms that is like noise and can only be made sense with filtering. The radar uses matched filtering as it knows exactly the characteristics of the radar signals it has sent (like frequency, PRF, modulation, pulse width). The EW receiver of course does not and must only guess the parameters and thus uses mismatched filtering. Even if the LPI signal is detected and stored, it is not that useful as the radar has already changed the signal parameters and the stored signal will not even give the radar extra work as it would not match the changed filters. AESA sets add the challenge of being able to quickly switch between every parameter at a moment’s notice and very randomly, which will put the jammer behind the radar
Jamming is likewise much more difficult against an AESA. Traditionally, jammers have operated by determining the operating frequency of the radar and then broadcasting a signal on it to confuse the receiver as to which is the “real” pulse and which is the jammer’s. This technique works as long as the radar system cannot easily change its operating frequency. When the transmitters were based on klystron tubes this was generally true, and radars, especially airborne ones, had only a few frequencies to choose among. A jammer could listen to those possible frequencies and select the one to be used to jam.
Most radars using modern electronics are capable of changing their operating frequency with every pulse. An AESA has the additional capability of spreading its frequencies across a wide band even in a single pulse, which equates to lowering the emission power, making jammers much less effective. Although it is possible to send out broadband white noise against all the possible frequencies, this means the amount of energy being sent at any one frequency is much lower, reducing its effectiveness
http://self.gutenberg.org/articles/aesa_radar
AESA radar characteristics such as random scan pattern, random frequency, random PRF all make it very resistance to DFRM deceptive jamming.
In general, high PRF radars are more resistant to ECM because their average power is greater. Changing the PRF in a random fashion is an effective counter to deception because deception ECM depends on predictability of the radar. However, because PRF is related to the basic timing of the radar, this technique results in additional complexity and expense. Random PRF has been employed as a very effective ECCM feature in some radars for many years and has the additional benefit of elimination of MTI radar blind speeds.
Scan pattern. The radar scan pattern can influence ECCM capability because it influences the amount of energy directed toward the radar target. An active tracking phased-array radar is quite ECM resistant because of its ability to rapidly scan its radar beam in a random fashion than in the regular circular or sector scan pattern of conventional radars. This irregular beam positioning would give the opposing ECM system little or no warning and make it impossible to predict where and when to transmit false signals. In systems where scanning is performed in the receiver rather than in the transmitted beam, such as those mentioned in the section on angle deception, ECM has no direct access to the radar scan pattern and thus has difficulty using that information to interfere with the radar system operation.
Frequency. Frequency agility is a significant ECCM design feature. Using components such as frequency synthesizers (something like those employed in radio scanners) instead of conventional crystal-controlled oscillators, some radars are able to change frequency within one pulse repetition time (PRT). This makes deception and jamming very difficult. The radar can be designed to change frequency automatically within a certain range, or this can be done manually.
http://fas.org/man/dod-101/navy/docs/fun/part11.htm
it was revealed by the RAAF a few months back in testimony to the Australian Parliament that DRFM jammers can be defeated easily by AESA radar
Air Marshal Brown: I think if you have a look around on an F16 sometimes that is not wonderful either. But getting back to the situational awareness, the ability to actually have that data fusion that the aeroplane has makes an incredible difference to how you perform in combat. I saw it first hand on a Red Flag mission in an F15D against a series of fifth-generation F22s. We were actually in the red air. In five engagements we never knew who had hit us and we never even saw the other aeroplane at any one particular time. That is a current fourth-generation aeroplane.
The data fusion in the stealth makes such a difference to your overall situational awareness it is quite incredible. After that particular mission I went back and had a look at the tapes on the F22, and the difference in the situational awareness in our two cockpits was just so fundamentally different. That is the key to fifth-generation. That is where I have trouble with the APA analysis. They tend to go down particular paths in the aeroplane, whether it is turn rate performance or acceleration. These are all important factors, but it is a combination of what you have actually got in the jet and the situational awareness that is resident in the cockpit of a fifth-generation aeroplane that makes the fundamental difference…To me that is key: it is not only stealth; it is the combination of the EOS and the radar to be able to build a comprehensive picture. In that engagement I talked about at Nellis, in Red Flag, the ability to be in a cockpit with a God’s-eye view of what is going on in the world was such an advantage over a fourth-generation fighter—and arguably one of the best fourth-generation fighters in existence, the F15. But even with a DRFM jamming pipe, we still had no chance in those particular engagements. And at no time did any of the performance characteristics that you are talking about have any relevance to those five engagements .
Another kind of jamming that work well even again the most sophisticated AESA radar are broadband noise jamming, because it is basically just like blind enemy receiver with overwhelming noise signal ( think of it like shinning a very bright light at some one so they cant see), however stealth fighter have significant advantage in this case due to their tiny RCS
http://www.rfcafe.com/references/electrical/ew-radar-handbook/radar-cross-section.htm
IRST in semi decent contitions can spot and track targets from 40-90km depending on aspect ratio and the potential use of afterburners.
according to Typhoon pilot their PIRATE can detect a supercruise F-22 from 50 km ( head on)
Assuming the pilots are retards flying at low alt from the moment they leave the tarmac.
how do they know when to flying low though ? if they flying high from the start then they would be detected from very far away
And that goes both ways. Shooting a target at low alt (as I took as an example for the ingress only) will reduce the range of the aggressors missiles as well.
Missiles launched from higher altitude can trade potential energy for more kinetic energy while the one launched from aircraft fly at low altitude will have to fight again gravity so they may not even able to reach target
the AMRAAM-ER for example is an improvement of AMRAAM with more than 4 times the range ( due to much bigger size, actually an ESSM fitted with the guidance section from the AIM-120) , when launched from ground, it’s ceiling is only 45k ft
i really cant imagine how a MICA or AIM-120 launched from sea level can reach an F-35 crusing at 40K ft let alone have enough energy to turn, , especially when considering that air at sea level is very thick, motor burn time is around 5-6 secs, thus missiles launched from sea level cant accelerate to speed as fast as the one launched at high – medium altitude , thus their ability to climb will be worse ( it easier for a missiles launched from 40K ft to zoom climb to 60K ft than the one launched from sea level to climb to 20Kft)
Also, flying low does shorten the radar detection range because of the amount of clutter.
agree, but clutter doesn’t shorten radar range as much as a delicate VLO design
Either you gain the advantage of a surprise atack (in which case energy state doesnt matter since the climb is over in less than a minute) or you go in at high altitude with good energy state and excellent range potential.
how exactly to you have surprised attack though? , do you think normal aircraft will suddenly gain radar detection range advantage again stealth fighter just because they flying low?
and iam pretty sure fighter can launch most of their missiles in a few seconds, so 1 minutes climbing is still too much time
Lets see how often that has happened….
The last incident was a Mirage in 1995. Thats like what, 20 years ago? I think the risk is acceptable. Sure, there have been some propeller aircrafts and helicopters as well but no fast jets.
last jet shot down by dogfight is even older than that
Excluding the engine.
And god knows what other items are required to actually fly the plane.
can you provide any source to support that statement
In theory the F35 is perfect, assuming that BVR missiles can’t be jammed.
This will motivate operational costs (including capital costs) of 2-3 times that of the competition.
If the missiles had a Pk of over 50% against jamming targets then it’s all good.
But in reality, just looking at whats out there now, the base Pk is less than 50% in a jammed environment. With systems like BriteCloud the missile also has multiple possible targets to choose from + much clutter. Since a normal fighter jet has a capacity of 36 stations with BriteCloud + 36 stations with chaffs + towed decoys one can assume that the missile will face at least 4 targets (3 decoys + actual target).
In the absolute best case scenario the missile will have a Pk of 0.5 x 4 = 0.125 or 12.5%. In reality this is probably optimistic if the enemy has modern jammers. 12,5% is the Pk for the correct target in this case.
To add an extra layer we could also assume IRIS-T being used as a hard-kill countermeasure (it has the capability, but the actual performance is not known). This would be a last resort but it is still in the mix…
Most AAM also have ECCM capabilities themselves so the effectiveness of BriteCloud again Meteor, AIM-120D is also questionable, another thing is AAM can be supported by the launching aircraft through data link and it is alot harder to jam the aircraft radar compared to a missiles especially if that aircraft have AESA radar
AAM will also have AESA radar seeker in future making it much harder to jam them ( from what i know, Russian already making prototype of AESA seeker for R-77, Japan cooperate with MBDA to make a new version of Meteor with AESA seeker for their F-35)
And there is nothing say that future long range AAM cant have IIR seeker, we already have a few of them like MICA IR, NCADE, R-27 IR… etc, Israel also have a programme to convert their Sturner SAM to AAM, stuner have both EO and RF sensor.
P/s : i think most on battlefield most soldiers would prefer to have a gun than a bullet proof vest and a knife