Know Your 'Rafale'

charlie

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It's not what I read at those time. Turk use the international freq. Russian plane radio were not able to cope this freq. (maybe to avoid a russian pilot can communicate with NATO to go to west... ).

And if it's the case, that means or russian pilots didn't answered, or decided not to obey.
Radio was not the issue here I can vouch for it as I work with fighters radios (nato).Though there is a possibility that Russian aircraft was in different channel and he might have not heard it. As far as I can think off there were many ways the turk could have avoided this situation even if there was no radio communication.

The French, UK or US any sane state would have avoided this kind of situation, but the turks already decided what to do on that particular instance and they did.

I don't know why you are taking side of Turks when their own president chose to back off from that situation.

Do you think the french would have handled the situation the same way ?

Sorry I went to a page which was discussed long time ago. Please ignore my response.
 

smestarz

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Sure you can ask your boss slight increase of 50%, hope that works for you.
Based on all the points that you have given, now look back on the upgrade cost of 51 million a plane for Mirage 2000 , where as a Rafale comes at what 72 million for flyway cost? and that too with a Radar, and all the nice things you said... that all shows that there were HUGE kickbacks in Mirage 2000 upgrade..
Thank you for clarification which helped to give another conclusion

Su 35 different than Su27/30 ? same plan form, same config (without canards....). all is the same.

Rafale can carry 9.5 tons. Mirage 2000 : 6tons (ie more than 50% more. indeed, it is slight..... I will ask my Boss monday a sightly wage increase of 50% ... :laugh:)
Rafale 13/14 hard points. Mirage : 9 (ie 45 to 55% more)
Manoeuvrability, range : Rafale better or far better.
Radar : Rafale better. No OSF in the Mirage. No sat link in the Mirage. Not the same electronic suit....

There is only one thing less in Rafale : Max speed. In the missile aera, speed was considered by French air force a secondary advantage.
 

smestarz

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In recent case, it was reported that some US Special forces are operating in in Syria and some Syrian Su-24 were in that area, and the American air force planes "persuaded" the Syrians to not proceed further. Thus this confirms your point, that the Turks had well decided in advance what to do, Further Su-24 does not have A2A weaponry, nor was it going to paint F-16 with its radar and lock on that the Turk F-16 feels threatened.

Radio was not the issue here I can vouch for it as I work with fighters radios (nato).Though there is a possibility that Russian aircraft was in different channel and he might have not heard it. As far as I can think off there were many ways the turk could have avoided this situation even if there was no radio communication.

The French, UK or US any sane state would have avoided this kind of situation, but the turks already decided what to do on that particular instance and they did.

I don't know why you are taking side of Turks when their own president chose to back off from that situation.

Do you think the french would have handled the situation the same way ?

Sorry I went to a page which was discussed long time ago. Please ignore my response.
 

BON PLAN

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Air Frame different, engines, avionics, more nos of pylons.. different radar..
show me the difference in the airframe please ?

upload_2016-8-22_8-33-36.jpeg
SU27

upload_2016-8-22_8-33-50.jpeg
SU35

Engine : thrust evolved from 12.3 to 13 tons. +5.5% .... OK.

Avionic, radar : I don't know. But surely improved ones.
 

BON PLAN

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Su-35S and Su-27S...
Yeah, the same but the completely different airframe inner structure twice encreased lifetime, 3 tons lighter and 2 tons of fuel extra :)
Different intakes, nose section and wing with optimal deformated centerline surfaces :)

Отправлено с моего XT1080 через Tapatalk
Your Brother Smestarz would say : it's like Mirage 2000 is just an evolution of Mirage 3 !
 

BON PLAN

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You don't need an digital radio to communicate in international frequency as they are in analog frequency and all digital radio have conventional mode.

When we test a radio we normally put the aircraft radio in conventional mode and then test it.
So explained me (you and the russian planes lovers) why the Su24 doesn't heard the message sent by the Turkish F16 .....
 

BON PLAN

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Radio was not the issue here I can vouch for it as I work with fighters radios (nato).Though there is a possibility that Russian aircraft was in different channel and he might have not heard it. As far as I can think off there were many ways the turk could have avoided this situation even if there was no radio communication.

The French, UK or US any sane state would have avoided this kind of situation, but the turks already decided what to do on that particular instance and they did.

I don't know why you are taking side of Turks when their own president chose to back off from that situation.

Do you think the french would have handled the situation the same way ?

Sorry I went to a page which was discussed long time ago. Please ignore my response.
Bro, You answered today to a quite old post of mine ! Between the political situation changed. Haven't you notice it ???
 

BON PLAN

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Sure you can ask your boss slight increase of 50%, hope that works for you.
Based on all the points that you have given, now look back on the upgrade cost of 51 million a plane for Mirage 2000 , where as a Rafale comes at what 72 million for flyway cost? and that too with a Radar, and all the nice things you said... that all shows that there were HUGE kickbacks in Mirage 2000 upgrade..
Thank you for clarification which helped to give another conclusion
I don't know if there were kickbacks.
Maybe under this "officcial" deal, there was another "black" deal.... about nuclear reactor tech for submarine or.... a completely new electronic defensive suite (derivated from Spectra?) or onother thing.
Don't ask it to me. What are the indians observers saying about that?
 

Yumdoot

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Firstly, F-35 did fly and win again F-16 and F-15 too, so not just A-4 , so dont try to play it down by only saying A-4
Secondly, structure G limit is not the same as G limit due to lift , for example everyone know F-16 is a 9G airplane , does that mean it can turn 9G at all altitude , all condition ? NO , at 50K feet , will barely have enough lift to turn 3G and barely enough thrust to sustain more than 1 G

<snip>

And about Thrust/weight , it actually rather hilarious that internet fanboy always compare T/W of one plane with another and think that which ever have higher T/W is definitely better.
F-35 can be played down even without the A-4. :D

F-16 was the F-16D version with heavy loads. Nothing like a Rafale or Sukhoi. As I said the representative threats are already developing to a point where they bring loaded supercruise to their attack plan.

F-15E was IIRC not the WVR combat but some interdiction mission. And the F-15E did not come in with AWACS as they are usually expected and designed to operate and don’t have IRSTs. F-15 is a reasonable plane which could possibly have stood-in for Su-30s and PAKFAs. So the X-band radar failed to detect. Big deal! Is that the one you are talking about?

Also I don’t understand how that education about G load and TWR is relevant. I mentioned the structural limits for Rafale (11g) only to show that Rafale has the bigger wing, better TWR as well as the structural margin of safety to do whatever it wishes to. Unlike the F-35 which must bring down the aggressor from its full operating capabilities. Su-35 type planes are doing even better in this regard.

I actually don’t mind it because I have come to accept that F-35 is a Strike fighter masquerading as an air superiority platform and the fanboys imagining air dominance capabilities.

Also you tend to give a lot of gratuitous theoretical education. Thanks for that effort but I am quoting facts. Mostly admitted facts. And I know which side to err on when faced with a choice between theory and facts.


If you want a fair T/W comparison , you need to equalize the range or afterburner combat time, a 500 km combat radius may mean half the internal tank for F-35 but that would mean full internal fuel tank for F-16 or Rafale
For Example what do you want to say with the above? That if the F-35 faces off with say an F-16D in real world then the F-16D must first come with disabilities that will change its combat characterstics to a level that F-35 can manage?

F-35 could have chosen to go with lesser fuel to the tests, if it needed better TWR instead of asking the F-16D to load up with extra load that the F-16D did not need at all for the WVR combat.

Or is it that the F-35 would not have fared any better despite dropping fuel load for a WVR test and the only option left was to load up the F-16D. Is it that the F-35 must load up on fuel because after all that is what it is made for – heavy internal carriage which make it stubbier and unsuitable for WVR combat.

And why must the F-35 load up so much fuel – because it is a known and admitted fact (before some house committee) that F-35 fuel burn is nearly 60% higher than that of F-16C. End result of trying too much.

So how do you fix the tests:
Step-1 - don’t bring in the F-16C which is actually much better representative of Rafale. Bring in the fatter F-16D.
Step-2 – force the F-16D further to carry extra load to make its wing loading match that of F-35.


Did you just said Rafale have performance close to the P-42 ? Do you know what it is
it is a fully stripped down Flanker without Radar , ECM ,IRST , IFF , paint , pylons and a modified engine T/W of 2 with full fuel load, no fighter flying today can excess the pure climbing performed of P-42 , and i mean it ,not even the F-22 or PAK-FA can do that.( the same go for Streak Eagle ) So no Rafale , Su-35 do not come close to it , not at all. Supercruise is irrelevance here since it just the matter of dynamic dry thrust at high speed.
They dropped 2 tons of weight and added probably 10% extra thrust.

You do the same to Rafale it will work nearabout. Do that to F-22 and it will most likely exceed all of them.

But F-35 even with similar changes will not. F-35 is a fat flying pig.


And where exactly did it say F-35 have to use full afterburner before start the 150 nm supercruising ?
or did you literally made that up ?
Would not the F-35 be a real super-cruiser already if it could reach 1.2 mach on dry thrust alone?

Why would then the Lockheed official talk about 150nm supercruise limit? Why not just say that the full range in super-cruise is X km?


all they said is :

The radar transmitter can be shut down in selected subsectors while the receivers continue to receive and process data. This is an effective feature in a jammed (ECM) environment. A single accurate line
(strobe) passing through the location of each jammer
is generated on the display console.


Do you know what the line mean ? , it literally mean you have no range gate of target , which mean the massive radar is nothing more than a RWR now , and it not surprise at all that RWR will see jamming signal just like they can see radar
I had warned you not to concentrated too much on the strobe which is meant for display purpose only. Still you are stuck with a display functionality.

Ok bhailog you decide.

Given that the Northrop claim is that the strobe is accurate to at least the Subsector level location of a Jammer, so the only thing missing would be the range. The subsectors within a Sector search were allocated by the AWACS itself.

Further given that Northrop also claims that only the radar transmitter is shut down and only towards that particular sub-sector where a Pelena-1 equivalent may be (MALD-J is irrelevant).

Further given that all receivers work full time (no exemption even for the jammer subsector).

Now in order to get the range information would it be too difficult to:
1) have that sub-sector searched by an X-band radar on the escorting fighters (mind you all types of sensors already have their own boresight line of sight fully stabilized and quantified); or
2) to generate an artificial aperture by keeping track of that subsector over time (if there is no fighter escort available).

Keeping track of Jammer bearings is also mentioned with the Vostok-E (see image below, that you asked for). Does that also imply that the Vostok-E has also deteriorated into a Radar Warning receiver?

No master ji, you are mistaken. And this is old technology, may be 70s for USA and 80s for rest of the world.


When i said track , i mean you can have an angular, velocity and range gate of target.Not just that you know the general direction.
How does it matter if the jammed AWACS is not able to range one solitary jammer or anything flying under the jammer’s cover when the current scenario is of:
1) abundance of sensors (IR/EO and Low Bands) and
2) every single fighter in a group with its GPS coordinates known and
3) each with its own boresight known and
4) an AWACS level processing power available at multiple points, in air or on ground.

You have to worry about the day when you don’t even need an AWACS to process the information and the same is readily done by every non-stealthy Su-30MKI or Rafale. Or the day when one or two small stealthy UAVs each with its own IR/EO sensor joins the fight.


The clutter rejection of AWACs is nothing similar to active cancellation
Clutter rejection of radar based on doppler gate and range gate
Active cancellation of Spectra based on destructive interference
They are nothing similar in any ways
Active cancellation and Spectra !
Master ji, in my several years of stay on this site I have never talked about Spectra and only hinted at Active cancellation once. Absolutely never were these even raised to you.

Look if you want me to admit you are smart then I will say it out loud for all people here:

HEY WORLD, PLEASE NOTE @ StealthFlanker IS SMART.



Did you just posted a picture of towed sonar array as an evidence to " multi static arrangement improved range " ???
Duh man! Do you want to make my arguments for me? Will I allow that?

And no, it was only for Bi-static. I specifically mentioned that. Multistatic will be many many more times better ranged because the reception is not going to be equally bad in all directions.

But look closely ASO is monostatic but the with the same source and a bigger isolated receiver of TASO the picture change completely. ASO and ACTAS serve as the lower and upper bounds for what is possible with several different ingredients thrown in. But the Bistatic arrangement clearly shows that there is a component increase due to bistatic arrangement.

In the case of radars say Nebo VHF, only the transmitter needs to be safe and protected. The receiver could be right under or even behind the F-35. I would work in such a case just like the Barrier-E FSR, only working at much higher peak powers. Barrier-E was designed for detection Spans of about 25-30 km. You can guess what the Nebo-VHF is going to do.


a towed sonar array have longer range than an internal sonar array not because they are in a multistatic arrangement but because the sonar is far aways from the clutter source ( the noise of the ship carrying it ) , another point is a towed sonar array can be bigger and be put below the reflective layer.
Also lower frequency tend to travel longer because the attenuation will be lower again them
Master ji, thank you for education but what do I do with this gratuitous education now.

“noise of the ship”! Aapko kanhi direction of motion dikh raha hai picture mein. Atlas Electronik people were careful enough to have metioned that the diagram is not not to scale but they forgot to mention whether the ship is producing noise or not?

It is obvious that when reasonable people make diagrams to show comparisons they do just that and go on and on about unrelated matters.


and as i said before , these direct will be ver far from frontal direction , so for your multistatic arrangement to be effective , the transmitter and receiver need to be stationed very far from each other.
And in normal operating conditions is that difficult?


And what will stop F-35 from go hunt these AWACs first ? , and you dont always know what targets will these F-35 will target either
Nothing theoretically speaking, except may be a bunch of better armed, better informed, fighters like Sukhois and Rafales with much better fighting capabilities.

With an AWACS around you can simply forget that an F-35 would get to approach even 300 km towards the AWACS.

BTW is there an internally carried Anti-Radiation Missile also in the works for F-35?




This says a 30 degree broadside all right but not about +-30 for a total of 60 degrees or +-15 for a total of 30. IIRC the F-35 is LO in the frontal sector right upto +-70 degrees.

Anyhow this itself constitutes an interesting input. If the Typhoons did in fact for a multistatic arrangement with a singular AWACS, it implies that the Typhoons have the receivers for the S-Band transmitted energy. Which leaves us with the quaint question is the L-Band antenna on PAKFA an IFF really. There is a lot of Cows being denounced as Goats.

The X band transmission by Typhoons would be practically useless in most cases for a multistatic arrangement.

If however there are no S-Band receivers on Typhoons then how was the multistatic arrangement established. Is it a lie? Or someting different from what is understood. AWACS could easily have vectored the Typhoons all through without the multistatic being invoked at all. While the mention of 25 to 30 degree separation could be the minimum/maximum parameters for operational reasons (the study was an internal simulation study only and nowhere does it state that the simulation involved multistatic radar capabilities)

Or is it that a simultaneous claim of use of multistatic arrangement, AWACS and Tyhoons are suggestive of even IRST &/or S-Band mixed triangulation.

In any case this states that the 4 Typhoons were successful in intercepting 8 F-35 and that some sort of multistatic arrangement was actually used which basically supports the claims being made about the approach Russians have taken.


No , the point is the AWACs radar , need to be stationed 30 degrees from the nose of F-35 because that where spike located , it doesnt matter what direction the AWACs facing.
No, the Eurofighter official (Craig Penrice, a Typhoon pilot and marketing adviser) says and suggests nothing about the spike being at the 30 degree dogleg. ‘Can be defeated by’ cannot be read as that being the only approach, nor can it be read as being the most efficient approach. In fact clear contextualization using the words “F-35s most likely approach path” suggests that operational considerations dictated the decision to place the Typhoons at those angles.

What I am noticing is that you don’t actually read much of anything. You just skim through things without even focusing, looking out only for things that seemingly support your pre-conceived notions.


we come back to multi static radar issue again. Same problem
No, you are trivializing the whole concept.

People are trying to develop multistatic SAR, ISAR and range increases, netted radars, GPS radars and you are stuck with the 30 degree broadside argument that too without providing a real study. I have waited enough for your study. I doubt its very existence now. All you have given is a sparsely backed claim by a Eurofighter marketing official who does not even refer to a study about multistatics. In fact the only mention of study in the flightglobal report you provide is a modeling of the possible interceptions. Please either provide the study itself or accept that the information is not enough.


How is inversed square law related at all here?
<snip>
That why i said the receiver and transmitter need to be far from each other to get a big angular seperation.
Ok seems like you have already made up your mind about this. But so have I. :devil: So that leaves the other Bhailog out.

For those who are reading this is said in the context of my suggestion of L Band AWACS working with L-Band receiver equipped PAKFA taking advantage of, volume search vs. linear flight path, capabilities of AWACS vs F-35.

Bhailog now consider this, the range for a monostatic radar is a root 4 function. The range for a bi-static system (non-FSR) is a root 2 function. Obviously as the PAKFAs race towards the F-35 receiving the AWACS-radar-returns the reflect signal has to travel less and less. F-35 must now decide to either enter the merge with obvious disadvantages or to abort mission and return. At this time if the F-35 decides to return they will expose their 190 KN tail and that will be seen and triangulated on the IRST at more than 90 km, with the superior speed of PAKFA still on its tail.

Something like that is reportedly also attempted by the Typhoons with the help of AWACS, going by the link provided.

Stated to be something like this:


Su-30MKI can also do this except that the AWACS will have to work more because there are no L-Band receivers on Su-30MKI. But even Su-30MKI can use vectors from AWACS with the several available IRSTs and triangulate easily.

Now you guys decide the angular separation needed and range yielded.

Here are two a links for root 4 and root 2 calculations which will show how the radar range is affected due to this factor for any given radar equation:
http://www.squarerootcalculator.co/
http://www.calculatorsoup.com/calculators/algebra/fourthroots.php

Note :To calculate the radar range between monostatic and bistatic arrangement the number that is to be ultimately rooted off is the going to be the same, presuming all things being equal. Range difference can arise due to other factors too but the biggest factor is only this singular factor. And mind you the ranges they mention in the brochures normally is the monostatic range.

@StealthFlanker you are reading things in a very different manner from the way I am. I do not deny that angular separation is needed and helpful in some circumstances, but then you put both legs of the triangle at same distances. Angular separation can still be maintained should you need it, even if one side of the triangle is shorter (fighters) than the other (AWACS). And with AWACS or IRST, that is easy to achieve.

In fact even without the IRST there may be reason enough to suspect that merely the VHF+S-bands will be able to provide a good kill box. Here is what a professional Dr. Igor Sutyagin has said in a conference of professionals, published with no professional counters till date:


If the above is true then the F-35 could be in very real danger even for its primary and only role of Strike.


you dont launch your missiles before you get a firing solution , unless the target is only like 4-5 km aways then angular direction is ok.
Unless the guidance is command guidance+INS. Off course the fighter should still know where to lob the semi active AAM but the CW mode can come up only at the last 9/10 pings probably last 4/5 km at 3+ mach. Or if the Active Seeker itself comes on at the very last moment only to acquire the target, travelling almost all the time as a simple command guided rocket.

So that will leave very little time to react. And similarly will be case with F-35 trying to avoid SAGG of S-400 by flying low where the EOTS capabilities themselves will have to be sacrificed by F-35. F-35 or MALD-J will have difficulty even jamming because nothing is being transmitted in the first place in X-Band or Ka-band. And during these final moments the X-Band radar of the S-400 battery, with much more power at its disposal, will also light up for the final kill. Each part of the system falling in line just when its needed.

Flying higher will bring the IRST of Sukhoi/Rafale into play given the big F-135 engines and clearer weather.


How do you plan to get the same radar pulse from a radar with pencil beam to travel to all your receiver several km apart ? . Understand ? the beam will not cover all receivers for you to do accurate TDOA
After reflection it will travel. In any case the track beam need not even figure in all this because there is no need to use TDOA for triangulation. Only angles are needed which for systems equipped with boresight and gimbaled LOS is known in advance.

TDOA was meant only for showing that sound waves in multistatic arrangements is working well in several types.


Thirdly, MADL use Ka band which is a very high frequency , that mean much thinner beam for same aperture size , your receiver will not even within the beam to detect it, moreover , Ka band also have high attenuation so it wont go very far either.

Btw , if datalink is so easy to detect then how can your Rafale use TDOA or triangulation for passive ranging then ? how do you think multi static arrangement work ??
Yes and the receivers too can be a chain of several small Ka band antenna.

The TDOA and FDOA as you rightly pointed out would normally need same source (transmitted or reflected). With encoding of identification signals even a singular source would not be needed and all receivers would be receiving many different reflected waves from many different targets illuminated by many different transmitters and no transmitter truly jam-able, in the first instance even with barrage jamming. Jammers too have to sharpen their beam so they too suffer from the linear vs spherical disadvantages. These things have solid evolutionary history to build on and are further being refined for radars, at several places including Thales. So Rafale too will use it in time that is if they are not already using it (my info being late). Better to use this tech development path then to go all stealth.

If a receiver at all instances knows for every target the TDOA and FDOA and knows this from multiple different transmitters with accurate PNT information available easily, what stops the network from even imaging a target. Though targeting does not require imaging but what if they find applications for it in terms of say distinguishing highly complex decoys from real targets, what then? To distinguish normal decoys from targets you will not even require real imaging.

But why do you invoke TDOA at all for multistatic radar. I just mentioned TDOA in the context of Arty Sound Ranging and that part is done. Mere triangulation is enough for taking on F-35. Only range information is difficult to get and that too only in higher bands and that too only with the one-on-one merges. For the first detection you will require 2 platforms but for all (which could be hundreds) the later detections, you will get as many ranges from as many angles as there are platforms to calculate angles. The nature of the triangle itself dictates that. The Typhoons probably just did it going by your link, foiling 85% of the F-35 strike missions.

If the F-35 relies on its frontal LO advantage then it can be easily beaten by stationing IRSTs in Fence like manner (as in FSR). The F-35 may turn to engage any target and the other IRST will get a crisp picture of the tail pipe may be upto 100km (or even 150 km).

Master ji abhi to IRST apertures have not even started evolving. What will the F-35 or even F-22 do, once they do. And then what will happen when these big apertures also sport scanning capabilities.


the special part is that up until now datalink has been omnidirectional
There were both types available since long. US which is the biggest arms budget just used the kind they thought would be enough for their needs.

Besides you seem to be ok with omnidirectional datalinking being effective, so it should be very very effective in guiding AAMs too. Should it not?


And i find it rather hilarious that you dont have any problem believing that Spectra can jam all spectrum from 0.1 Ghz to 100 Ghz with it's tiny jamming antenna but suddently it a problem when MALD-J do that ?
I don’t care much for Spectra and MALD-J cannot jam AWACS.

So tell me what VHF radar decamp in 6 minutes ? official source please
Yes official from the manufacturer’s site.




The question here is what kind of target you have to face ? is it a ship with massive RCS ? is it a ballistics missiles with very high speed ( big doppler shift) ? or is it an aircraft with tiny RCS ? again high clutter background ?
Jane do that was an aside. People it was meant for must have understood.


Yumdoot said:
Won’t the MALD standin for the NPI F-35. Are we increasing the foot print or decreasing it this week
iam even sure what you are trying to say here ?
MALD-J will off course work against Active seeker heads. That is its main use. It probably may also have X-band capabilities because the Americans are ahead of all in this kind of dual band arrays. So MALD-J may also work against FCR of fighters. But this will affect only those air forces who are relying still on improving their X-band FCR to be able to work against LO targets like the Swedes. For those relying on MIMO multiband radars and IRST this will have nearly no use.

The Americans are thinking is that they should spoil the end game for all SAMs/AAMs hence their focus on DIRCM and Standin jamming. Essentially they have already conceded that jamming at long distances is not useful or practicable. While SAMs and AAMs will evolve again to take this into account there may be entirely new technologies that will facilitate this evolution.


I didnt say permanent but they rarely move. And NEBO aperture is nearly 3 time the size of Vostok E to be honest. Btw where is source ?
Master ji, NEBO aperture even if 3 times larger can be managed in much the same way as Vostok-E. Only bigger trucks will be required alongwith stated needs of the militaries.

But where is the need to move them as often?

Why not just put up even more fixed decoy antenna at suitable distances. What do these rods, pipes and whip/yagis antennas even cost. 90% of the antenna array is composed of empty spaces. These have been made for ages. And unless the Anti-radiation missile is able to distinguish the movable antenna from the decoys, the movement is not even needed.

Besides I have linked the Vostok-E image above in the process of folding up. To me it looks like even the 6 minute time can be beaten. The Nebo VHF currently is stated at 20 minutes and while it is certainly bigger than Vostok-E you always have the option of redesigning the stowage for faster folding.

The real radar is the computing vehicle with all the computers. That is the costly one and that one is silent, camouflaged and can further be protected by close in weapon systems.


so we changed from Rafale to Vostok E now ? , and why put an ground early warning radar in when we are talking about air combat and firing solution ?
See Vostok-E came in because you wanted a link. But why not. French VHF surveillance practice is nothing to scoff at. Only lesser budget and different needs stop them. Besides they seem to be happy with S-band radars for AD surveillance. Almost the same as us. Could be that with merely the S-band coverage they already have figured out how to make a robust OODA loop.


That is just dumb to be honest , dont you know that low frequency can actually be reflected from the ionoshpere or that even the small things like chaff can have very high RCS at low frequency ?
The difference FOPEN designers were making was about man made decoys (including chaff) and just leaves, trees, rain, hail and bad weather – while compared in the X band and UHF/VHF.

Why do you bring the chaff along in this argument. Though why not even that is man made, only its not going to be very persistent.

I personally don’t mind chaff for lower bands either. Actually I don’t mind any jamming at all, speaking from an defenders perspective. Jamming of any kind implies there is something interesting to be found.

In fact the difference is stark even if the systems are from the same countries. American have for long operated VHF long range sensors for space applications. There X band ICBM watcher however failed. Both being as of today.

Cant you read the formula and the sentences in the pic ????? Do you understand what is burn through distance and radar equation ???????????
Who is challenging you on your radar burn throughs?

Do I look like I care for that?

And besides it is you who is being unfair and doubting Sepctra even though it carries the same tech. (an old tech.) for radar waveform cancellations only at a lesser distance (which BTW also implies smaller formfactors for Spectra hardware).

Besides it is you who does not want to acknowledge that for bistatic arrangements the range increases merely because the waves don’t have to travel back as far and this return path distance could be closing in at Mach 2 or 3+. The exact same reason why Jammers are effective in the first place. And further that the range increases are way more than a mere doubling of ranges.

While for ‘Jamming vs. Jamming burn through’ it is a simpler issue because both transmissions are towards each other. Which is also why the French are claiming that they have spent close to 25% of Rafale development cost in making the Spectra which will analyses the radar from the first transmission itself and will have a big library of all waveforms that the F-35 cannot change easily. The jammer OTOH will not even know if it has been taken care of and will continue to announce its presence in all but range. You will basically be detected long long before you can even bring your MALD-J into consideration, which in any case cannot jam any sensors that are not already discounted.

You do get redundancy by MALD-J but what is the point if you can be seen all of EM spectrum except the X-band.


No one say they are dumb , IFF is very important , internet fan boy who think L band of that size can be used as fire control radar that are dumb
So you highness allows for the IFF to retain its importance without answering the main question as to why would the Russians need their interrogators to be this big when the whole world is doing it differently? Detection and targeting of a LO target is a challenge but how is interrogation a challenge?

And besides IFF involves some of the same waveform management techniques that for radars and jammers require and that leaves your objection regarding aperture size only. Which is suitably discussed elsewhere herein.

And even if these are just IFF for really long range interrogations then, how do you think it helps if the F-35 is showing up on the VHF and L-band but not on the X-band and is either not responding or improperly responding to such large range IFF challenges. How would you classify such an interrogation? At such long ranges if the F-35 is classified as a high probability adversary then does it not help the defender?

And I don’t understand your insistence that the L Band radar on PAKFA cannot be used for FCR. Well ok, a true fire control will be difficult but what about merely keeping the range information fed to the AAM. Why must it fail in that. A capability which is over and above the capability of that array, to act as a homing head for the whole aircrafts basis the radar emissions of the L Band AWACS.

Why the hell would Russians use this big IFF? Are they dumb.

So you have no valid arguement rather than that half ass sacrcasm ?? so what make you think US and many country that bought F-35 are dumb ???
Because it’s a habit by now. Most people buying F-35 today had a healthy lead in all the anti-VLO technologies. Today they allowed their own lead to peter away for F-35.

I don’t mind it.

Americans have always tried to put roadblocks in the path of others which is the only way they have grown ‘powerful’. They first developed the nuke then made lots and lots of them, then tried to keep everybody else out of it. Some succumbed to their tactics. Some did not. At least 3 billion people on the planet dd not give in. It is the same with every piece of technology.


1) the jamming part is done by MALD-J which is disposable asset
2) no one turn on their jammer randommly , no radar pulse received then no jamming turn on
3) one F-35 that was transmitted can share information with group of F-35 so your silent PAK-FA and Rafale will be practically blind again the whole F-35 formation ( dont get this wrong i see PAK-FA as an awesome asset too )
1) Expendable, towed, integrated whatever. Hardly matters. There are more than enough ways to know range and send in the AAM. MALD-J will be effective in only the front sector and only against Active seeker heads. The semi actives and SAGG won’t even reveal themselves till the very last moment. The future will see even better warheads on these missiles.

2) Hardly matters, the Jammer can be put doing in its bearings and only the range needs to be worked at which can be done off board. There were times when the height component too had to be calculated separately and automation of this much technology is not difficult.

3) I don’t deny that F-35 too can share information which is how it is ultimately going to be. As I said PAKFA or Su-30MKI or Rafale need not be silent at all. The silence is merely because the X band radar is not as useful and not because Stealth is a method of fighting with these aircrafts. All aspect stealth is American contribution to the world. The world never believed in it and that is why the world has take only the relevant portion of shaping and RAMs for a limited frontal stealth which will be used only in the attack modes, not in hunter modes.


I didnt say PAC-3 dont work , dont try to troll to win your argument , i said TVC doesnt help the big resolution cell problem.
Don’t look like big kill boxes if you go by, what the professionals are discussing among themselves (refer Dr. Igor Sutyagin in RUSI conference, linked above)


You mean like the same way Russian throw a tantum when US put PAC3 near their border ? it just a politics thing.
Which is backed by extant technology. Nobody begrudges S-200 or Dvinas or even early generation Patriots.
 

gadeshi

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show me the difference in the airframe please ?

View attachment 9924SU27

View attachment 9925SU35

Engine : thrust evolved from 12.3 to 13 tons. +5.5% .... OK.

Avionic, radar : I don't know. But surely improved ones.
Different engine with 14,5 tons thrust each (not 13, 13 tons are Al-31F-M1 on Su-30SM and Su-34).
Completely different internal force sustain layout. It is inside, not outside.
Different intakes (parallax airflow compression scheme in addition to generic ramp-based one).
Different nose section.

Отправлено с моего XT1080 через Tapatalk
 

biswas_k11

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Russia is ready to tap India as a global aeronautics manufacturing base and is willing to partner local firms in developing production and
technological their capabilities in the aviation sector, an official representing a delegation from the country said during bilateral talks held here.
India, on its part, expressed eagerness to jointly develop iron ore and coal mines in Russian territory and sought technical inputs on producing high-grade cold-rolled, grain-power in used typically steel, oriented transmission equipment.
Ramesh Abhishek, secretary, department of industrial policy and promotion in the ministry of commerce and industry, led the bilateral talks held under the aegis of an India-Russia working group on modernization and industrial co-operation. The Russian delegation was headed by the trade and industry of minister deputy Alexander Potapov.
While both sides acknowledged their mutual interest in expanding bilateral cooperation between Russian and Indian companies in different sectors, more focused discussions mining, modernization,
on held were fertilisers and civil aviation. Civil aviation “In the civil aviation sector, Russian side declared its readiness to participate in the Make in India program in order to develop technological and production capabilities of the Indian side in this field and potential supplies of the jointly produced equipment to third countries,” according to a statement issued by the commerce and industry ministry.
The Russians also reiterated their interest in Russian of participation possible the companies in the Delhi-Mumbai Industrial Corridor.
In mining and metallurgy, the two sides agreed to exchange information on potential areas for co-operation in view of India’
 

biswas_k11

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Russia is ready to tap India as a global aeronautics manufacturing base and is willing to partner local firms in developing their technological and production capabilities in the aviation sector, an official representing a delegation from the country said during bilateral talks held here.

India, on its part, expressed eagerness to jointly develop iron ore and coal mines in Russian territory and sought technical inputs on producing high-grade cold-rolled, grain-oriented steel, typically used in power transmission equipment.

Ramesh Abhishek, secretary, department of industrial policy and promotion in the ministry of commerce and industry, led the bilateral talks held under the aegis of an India-Russia working group on modernization and industrial co-operation. The Russian delegation was headed by the deputy minister of industry and trade Alexander Potapov.

While both sides acknowledged their mutual interest in expanding bilateral cooperation between Russian and Indian companies in different sectors, more focused discussions were held on modernization, mining, fertilisers and civil aviation.

Civil aviation “In the civil aviation sector, Russian side declared its readiness to participate in the Make in India program in order to develop technological and production capabilities of the Indian side in this field and potential supplies of the jointly produced equipment to third countries,” according to a statement issued by the commerce and industry ministry.

The Russians also reiterated their interest in the possible participation of Russian companies in the Delhi-Mumbai Industrial Corridor.

In mining and metallurgy, the two sides agreed to exchange information on potential areas for co-operation in view of India’s request to develop coal fields and iron ore mines in Russia, according to the statement.
 

kstriya

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It's India which has selected Rafale, not the contrary.
Have a nice day Rafale heater.
Now that I am the official Rafale Heater:crazy: ( Not hater), I suggest we Indians drop the Rafale as a choice for MMRCA as it has already generated a lot of heated debate and friction between a lot of members here. I do not want to heat it any more, so lets drop it we can save some trauma for the DFI readers who are just waiting for this deal to be scrapped.:hail: But surely you will be the cry baby in sometime:crying: and as a customer, we Indians will have the last laugh:hippo:
 

BON PLAN

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Now that I am the official Rafale Heater:crazy: ( Not hater), I suggest we Indians drop the Rafale as a choice for MMRCA as it has already generated a lot of heated debate and friction between a lot of members here. I do not want to heat it any more, so lets drop it we can save some trauma for the DFI readers who are just waiting for this deal to be scrapped.:hail: But surely you will be the cry baby in sometime:crying: and as a customer, we Indians will have the last laugh:hippo:
Unfortunately, India will acquire Rafale soon.
Why?
- Because if Rafale was so inadequated, why last year your PM requested 36 in a quick delivery schedule? It was so easy to say nothing and scratched the MMRCA project saying the DA bid was not realist, as UAE did some years ago. MMRCA was canceled. But a Rafale deal initiated by Modi....
- Because the IAF is declining. Tejas is far from beiing massively induce (hand made to day) and not war ready until some long years. Su30 : you can't rely too much on a single plane, especially a so bigger one. No other plane are on the line of sight, and negotiating with Boeing, Saab, LM... take time, especially in India (remember it took 22 years to firm the Hawk deal. Tanker deal is a ping pong game between russian, european and indian side. Light helo.... ).

So I'm convinced the last to laugh will be.... my self :) And I'm sure some of the Rafale haters gang (and not heaters, sorry for that) know that also. :confused1:

Just wait some weeks. Saying until the end of the year
 

BON PLAN

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F-35 can be played down even without the A-4. :D

F-16 was the F-16D version with heavy loads. Nothing like a Rafale or Sukhoi. As I said the representative threats are already developing to a point where they bring loaded supercruise to their attack plan.

F-15E was IIRC not the WVR combat but some interdiction mission. And the F-15E did not come in with AWACS as they are usually expected and designed to operate and don’t have IRSTs. F-15 is a reasonable plane which could possibly have stood-in for Su-30s and PAKFAs. So the X-band radar failed to detect. Big deal! Is that the one you are talking about?

Also I don’t understand how that education about G load and TWR is relevant. I mentioned the structural limits for Rafale (11g) only to show that Rafale has the bigger wing, better TWR as well as the structural margin of safety to do whatever it wishes to. Unlike the F-35 which must bring down the aggressor from its full operating capabilities. Su-35 type planes are doing even better in this regard.

I actually don’t mind it because I have come to accept that F-35 is a Strike fighter masquerading as an air superiority platform and the fanboys imagining air dominance capabilities.

Also you tend to give a lot of gratuitous theoretical education. Thanks for that effort but I am quoting facts. Mostly admitted facts. And I know which side to err on when faced with a choice between theory and facts.




For Example what do you want to say with the above? That if the F-35 faces off with say an F-16D in real world then the F-16D must first come with disabilities that will change its combat characterstics to a level that F-35 can manage?

F-35 could have chosen to go with lesser fuel to the tests, if it needed better TWR instead of asking the F-16D to load up with extra load that the F-16D did not need at all for the WVR combat.

Or is it that the F-35 would not have fared any better despite dropping fuel load for a WVR test and the only option left was to load up the F-16D. Is it that the F-35 must load up on fuel because after all that is what it is made for – heavy internal carriage which make it stubbier and unsuitable for WVR combat.

And why must the F-35 load up so much fuel – because it is a known and admitted fact (before some house committee) that F-35 fuel burn is nearly 60% higher than that of F-16C. End result of trying too much.

So how do you fix the tests:
Step-1 - don’t bring in the F-16C which is actually much better representative of Rafale. Bring in the fatter F-16D.
Step-2 – force the F-16D further to carry extra load to make its wing loading match that of F-35.




They dropped 2 tons of weight and added probably 10% extra thrust.

You do the same to Rafale it will work nearabout. Do that to F-22 and it will most likely exceed all of them.

But F-35 even with similar changes will not. F-35 is a fat flying pig.




Would not the F-35 be a real super-cruiser already if it could reach 1.2 mach on dry thrust alone?

Why would then the Lockheed official talk about 150nm supercruise limit? Why not just say that the full range in super-cruise is X km?




I had warned you not to concentrated too much on the strobe which is meant for display purpose only. Still you are stuck with a display functionality.

Ok bhailog you decide.

Given that the Northrop claim is that the strobe is accurate to at least the Subsector level location of a Jammer, so the only thing missing would be the range. The subsectors within a Sector search were allocated by the AWACS itself.

Further given that Northrop also claims that only the radar transmitter is shut down and only towards that particular sub-sector where a Pelena-1 equivalent may be (MALD-J is irrelevant).

Further given that all receivers work full time (no exemption even for the jammer subsector).

Now in order to get the range information would it be too difficult to:
1) have that sub-sector searched by an X-band radar on the escorting fighters (mind you all types of sensors already have their own boresight line of sight fully stabilized and quantified); or
2) to generate an artificial aperture by keeping track of that subsector over time (if there is no fighter escort available).

Keeping track of Jammer bearings is also mentioned with the Vostok-E (see image below, that you asked for). Does that also imply that the Vostok-E has also deteriorated into a Radar Warning receiver?

No master ji, you are mistaken. And this is old technology, may be 70s for USA and 80s for rest of the world.




How does it matter if the jammed AWACS is not able to range one solitary jammer or anything flying under the jammer’s cover when the current scenario is of:
1) abundance of sensors (IR/EO and Low Bands) and
2) every single fighter in a group with its GPS coordinates known and
3) each with its own boresight known and
4) an AWACS level processing power available at multiple points, in air or on ground.

You have to worry about the day when you don’t even need an AWACS to process the information and the same is readily done by every non-stealthy Su-30MKI or Rafale. Or the day when one or two small stealthy UAVs each with its own IR/EO sensor joins the fight.




Active cancellation and Spectra !
Master ji, in my several years of stay on this site I have never talked about Spectra and only hinted at Active cancellation once. Absolutely never were these even raised to you.

Look if you want me to admit you are smart then I will say it out loud for all people here:

HEY WORLD, PLEASE NOTE @ StealthFlanker IS SMART.




Duh man! Do you want to make my arguments for me? Will I allow that?

And no, it was only for Bi-static. I specifically mentioned that. Multistatic will be many many more times better ranged because the reception is not going to be equally bad in all directions.

But look closely ASO is monostatic but the with the same source and a bigger isolated receiver of TASO the picture change completely. ASO and ACTAS serve as the lower and upper bounds for what is possible with several different ingredients thrown in. But the Bistatic arrangement clearly shows that there is a component increase due to bistatic arrangement.

In the case of radars say Nebo VHF, only the transmitter needs to be safe and protected. The receiver could be right under or even behind the F-35. I would work in such a case just like the Barrier-E FSR, only working at much higher peak powers. Barrier-E was designed for detection Spans of about 25-30 km. You can guess what the Nebo-VHF is going to do.




Master ji, thank you for education but what do I do with this gratuitous education now.

“noise of the ship”! Aapko kanhi direction of motion dikh raha hai picture mein. Atlas Electronik people were careful enough to have metioned that the diagram is not not to scale but they forgot to mention whether the ship is producing noise or not?

It is obvious that when reasonable people make diagrams to show comparisons they do just that and go on and on about unrelated matters.




And in normal operating conditions is that difficult?




Nothing theoretically speaking, except may be a bunch of better armed, better informed, fighters like Sukhois and Rafales with much better fighting capabilities.

With an AWACS around you can simply forget that an F-35 would get to approach even 300 km towards the AWACS.

BTW is there an internally carried Anti-Radiation Missile also in the works for F-35?





This says a 30 degree broadside all right but not about +-30 for a total of 60 degrees or +-15 for a total of 30. IIRC the F-35 is LO in the frontal sector right upto +-70 degrees.

Anyhow this itself constitutes an interesting input. If the Typhoons did in fact for a multistatic arrangement with a singular AWACS, it implies that the Typhoons have the receivers for the S-Band transmitted energy. Which leaves us with the quaint question is the L-Band antenna on PAKFA an IFF really. There is a lot of Cows being denounced as Goats.

The X band transmission by Typhoons would be practically useless in most cases for a multistatic arrangement.

If however there are no S-Band receivers on Typhoons then how was the multistatic arrangement established. Is it a lie? Or someting different from what is understood. AWACS could easily have vectored the Typhoons all through without the multistatic being invoked at all. While the mention of 25 to 30 degree separation could be the minimum/maximum parameters for operational reasons (the study was an internal simulation study only and nowhere does it state that the simulation involved multistatic radar capabilities)

Or is it that a simultaneous claim of use of multistatic arrangement, AWACS and Tyhoons are suggestive of even IRST &/or S-Band mixed triangulation.

In any case this states that the 4 Typhoons were successful in intercepting 8 F-35 and that some sort of multistatic arrangement was actually used which basically supports the claims being made about the approach Russians have taken.




No, the Eurofighter official (Craig Penrice, a Typhoon pilot and marketing adviser) says and suggests nothing about the spike being at the 30 degree dogleg. ‘Can be defeated by’ cannot be read as that being the only approach, nor can it be read as being the most efficient approach. In fact clear contextualization using the words “F-35s most likely approach path” suggests that operational considerations dictated the decision to place the Typhoons at those angles.

What I am noticing is that you don’t actually read much of anything. You just skim through things without even focusing, looking out only for things that seemingly support your pre-conceived notions.




No, you are trivializing the whole concept.

People are trying to develop multistatic SAR, ISAR and range increases, netted radars, GPS radars and you are stuck with the 30 degree broadside argument that too without providing a real study. I have waited enough for your study. I doubt its very existence now. All you have given is a sparsely backed claim by a Eurofighter marketing official who does not even refer to a study about multistatics. In fact the only mention of study in the flightglobal report you provide is a modeling of the possible interceptions. Please either provide the study itself or accept that the information is not enough.




Ok seems like you have already made up your mind about this. But so have I. :devil: So that leaves the other Bhailog out.

For those who are reading this is said in the context of my suggestion of L Band AWACS working with L-Band receiver equipped PAKFA taking advantage of, volume search vs. linear flight path, capabilities of AWACS vs F-35.

Bhailog now consider this, the range for a monostatic radar is a root 4 function. The range for a bi-static system (non-FSR) is a root 2 function. Obviously as the PAKFAs race towards the F-35 receiving the AWACS-radar-returns the reflect signal has to travel less and less. F-35 must now decide to either enter the merge with obvious disadvantages or to abort mission and return. At this time if the F-35 decides to return they will expose their 190 KN tail and that will be seen and triangulated on the IRST at more than 90 km, with the superior speed of PAKFA still on its tail.

Something like that is reportedly also attempted by the Typhoons with the help of AWACS, going by the link provided.

Stated to be something like this:


Su-30MKI can also do this except that the AWACS will have to work more because there are no L-Band receivers on Su-30MKI. But even Su-30MKI can use vectors from AWACS with the several available IRSTs and triangulate easily.

Now you guys decide the angular separation needed and range yielded.

Here are two a links for root 4 and root 2 calculations which will show how the radar range is affected due to this factor for any given radar equation:
http://www.squarerootcalculator.co/
http://www.calculatorsoup.com/calculators/algebra/fourthroots.php

Note :To calculate the radar range between monostatic and bistatic arrangement the number that is to be ultimately rooted off is the going to be the same, presuming all things being equal. Range difference can arise due to other factors too but the biggest factor is only this singular factor. And mind you the ranges they mention in the brochures normally is the monostatic range.

@StealthFlanker you are reading things in a very different manner from the way I am. I do not deny that angular separation is needed and helpful in some circumstances, but then you put both legs of the triangle at same distances. Angular separation can still be maintained should you need it, even if one side of the triangle is shorter (fighters) than the other (AWACS). And with AWACS or IRST, that is easy to achieve.

In fact even without the IRST there may be reason enough to suspect that merely the VHF+S-bands will be able to provide a good kill box. Here is what a professional Dr. Igor Sutyagin has said in a conference of professionals, published with no professional counters till date:


If the above is true then the F-35 could be in very real danger even for its primary and only role of Strike.




Unless the guidance is command guidance+INS. Off course the fighter should still know where to lob the semi active AAM but the CW mode can come up only at the last 9/10 pings probably last 4/5 km at 3+ mach. Or if the Active Seeker itself comes on at the very last moment only to acquire the target, travelling almost all the time as a simple command guided rocket.

So that will leave very little time to react. And similarly will be case with F-35 trying to avoid SAGG of S-400 by flying low where the EOTS capabilities themselves will have to be sacrificed by F-35. F-35 or MALD-J will have difficulty even jamming because nothing is being transmitted in the first place in X-Band or Ka-band. And during these final moments the X-Band radar of the S-400 battery, with much more power at its disposal, will also light up for the final kill. Each part of the system falling in line just when its needed.

Flying higher will bring the IRST of Sukhoi/Rafale into play given the big F-135 engines and clearer weather.




After reflection it will travel. In any case the track beam need not even figure in all this because there is no need to use TDOA for triangulation. Only angles are needed which for systems equipped with boresight and gimbaled LOS is known in advance.

TDOA was meant only for showing that sound waves in multistatic arrangements is working well in several types.




Yes and the receivers too can be a chain of several small Ka band antenna.

The TDOA and FDOA as you rightly pointed out would normally need same source (transmitted or reflected). With encoding of identification signals even a singular source would not be needed and all receivers would be receiving many different reflected waves from many different targets illuminated by many different transmitters and no transmitter truly jam-able, in the first instance even with barrage jamming. Jammers too have to sharpen their beam so they too suffer from the linear vs spherical disadvantages. These things have solid evolutionary history to build on and are further being refined for radars, at several places including Thales. So Rafale too will use it in time that is if they are not already using it (my info being late). Better to use this tech development path then to go all stealth.

If a receiver at all instances knows for every target the TDOA and FDOA and knows this from multiple different transmitters with accurate PNT information available easily, what stops the network from even imaging a target. Though targeting does not require imaging but what if they find applications for it in terms of say distinguishing highly complex decoys from real targets, what then? To distinguish normal decoys from targets you will not even require real imaging.

But why do you invoke TDOA at all for multistatic radar. I just mentioned TDOA in the context of Arty Sound Ranging and that part is done. Mere triangulation is enough for taking on F-35. Only range information is difficult to get and that too only in higher bands and that too only with the one-on-one merges. For the first detection you will require 2 platforms but for all (which could be hundreds) the later detections, you will get as many ranges from as many angles as there are platforms to calculate angles. The nature of the triangle itself dictates that. The Typhoons probably just did it going by your link, foiling 85% of the F-35 strike missions.

If the F-35 relies on its frontal LO advantage then it can be easily beaten by stationing IRSTs in Fence like manner (as in FSR). The F-35 may turn to engage any target and the other IRST will get a crisp picture of the tail pipe may be upto 100km (or even 150 km).

Master ji abhi to IRST apertures have not even started evolving. What will the F-35 or even F-22 do, once they do. And then what will happen when these big apertures also sport scanning capabilities.




There were both types available since long. US which is the biggest arms budget just used the kind they thought would be enough for their needs.

Besides you seem to be ok with omnidirectional datalinking being effective, so it should be very very effective in guiding AAMs too. Should it not?




I don’t care much for Spectra and MALD-J cannot jam AWACS.



Yes official from the manufacturer’s site.






Jane do that was an aside. People it was meant for must have understood.




MALD-J will off course work against Active seeker heads. That is its main use. It probably may also have X-band capabilities because the Americans are ahead of all in this kind of dual band arrays. So MALD-J may also work against FCR of fighters. But this will affect only those air forces who are relying still on improving their X-band FCR to be able to work against LO targets like the Swedes. For those relying on MIMO multiband radars and IRST this will have nearly no use.

The Americans are thinking is that they should spoil the end game for all SAMs/AAMs hence their focus on DIRCM and Standin jamming. Essentially they have already conceded that jamming at long distances is not useful or practicable. While SAMs and AAMs will evolve again to take this into account there may be entirely new technologies that will facilitate this evolution.




Master ji, NEBO aperture even if 3 times larger can be managed in much the same way as Vostok-E. Only bigger trucks will be required alongwith stated needs of the militaries.

But where is the need to move them as often?

Why not just put up even more fixed decoy antenna at suitable distances. What do these rods, pipes and whip/yagis antennas even cost. 90% of the antenna array is composed of empty spaces. These have been made for ages. And unless the Anti-radiation missile is able to distinguish the movable antenna from the decoys, the movement is not even needed.

Besides I have linked the Vostok-E image above in the process of folding up. To me it looks like even the 6 minute time can be beaten. The Nebo VHF currently is stated at 20 minutes and while it is certainly bigger than Vostok-E you always have the option of redesigning the stowage for faster folding.

The real radar is the computing vehicle with all the computers. That is the costly one and that one is silent, camouflaged and can further be protected by close in weapon systems.



See Vostok-E came in because you wanted a link. But why not. French VHF surveillance practice is nothing to scoff at. Only lesser budget and different needs stop them. Besides they seem to be happy with S-band radars for AD surveillance. Almost the same as us. Could be that with merely the S-band coverage they already have figured out how to make a robust OODA loop.




The difference FOPEN designers were making was about man made decoys (including chaff) and just leaves, trees, rain, hail and bad weather – while compared in the X band and UHF/VHF.

Why do you bring the chaff along in this argument. Though why not even that is man made, only its not going to be very persistent.

I personally don’t mind chaff for lower bands either. Actually I don’t mind any jamming at all, speaking from an defenders perspective. Jamming of any kind implies there is something interesting to be found.

In fact the difference is stark even if the systems are from the same countries. American have for long operated VHF long range sensors for space applications. There X band ICBM watcher however failed. Both being as of today.



Who is challenging you on your radar burn throughs?

Do I look like I care for that?

And besides it is you who is being unfair and doubting Sepctra even though it carries the same tech. (an old tech.) for radar waveform cancellations only at a lesser distance (which BTW also implies smaller formfactors for Spectra hardware).

Besides it is you who does not want to acknowledge that for bistatic arrangements the range increases merely because the waves don’t have to travel back as far and this return path distance could be closing in at Mach 2 or 3+. The exact same reason why Jammers are effective in the first place. And further that the range increases are way more than a mere doubling of ranges.

While for ‘Jamming vs. Jamming burn through’ it is a simpler issue because both transmissions are towards each other. Which is also why the French are claiming that they have spent close to 25% of Rafale development cost in making the Spectra which will analyses the radar from the first transmission itself and will have a big library of all waveforms that the F-35 cannot change easily. The jammer OTOH will not even know if it has been taken care of and will continue to announce its presence in all but range. You will basically be detected long long before you can even bring your MALD-J into consideration, which in any case cannot jam any sensors that are not already discounted.

You do get redundancy by MALD-J but what is the point if you can be seen all of EM spectrum except the X-band.




So you highness allows for the IFF to retain its importance without answering the main question as to why would the Russians need their interrogators to be this big when the whole world is doing it differently? Detection and targeting of a LO target is a challenge but how is interrogation a challenge?

And besides IFF involves some of the same waveform management techniques that for radars and jammers require and that leaves your objection regarding aperture size only. Which is suitably discussed elsewhere herein.

And even if these are just IFF for really long range interrogations then, how do you think it helps if the F-35 is showing up on the VHF and L-band but not on the X-band and is either not responding or improperly responding to such large range IFF challenges. How would you classify such an interrogation? At such long ranges if the F-35 is classified as a high probability adversary then does it not help the defender?

And I don’t understand your insistence that the L Band radar on PAKFA cannot be used for FCR. Well ok, a true fire control will be difficult but what about merely keeping the range information fed to the AAM. Why must it fail in that. A capability which is over and above the capability of that array, to act as a homing head for the whole aircrafts basis the radar emissions of the L Band AWACS.

Why the hell would Russians use this big IFF? Are they dumb.



Because it’s a habit by now. Most people buying F-35 today had a healthy lead in all the anti-VLO technologies. Today they allowed their own lead to peter away for F-35.

I don’t mind it.

Americans have always tried to put roadblocks in the path of others which is the only way they have grown ‘powerful’. They first developed the nuke then made lots and lots of them, then tried to keep everybody else out of it. Some succumbed to their tactics. Some did not. At least 3 billion people on the planet dd not give in. It is the same with every piece of technology.




1) Expendable, towed, integrated whatever. Hardly matters. There are more than enough ways to know range and send in the AAM. MALD-J will be effective in only the front sector and only against Active seeker heads. The semi actives and SAGG won’t even reveal themselves till the very last moment. The future will see even better warheads on these missiles.

2) Hardly matters, the Jammer can be put doing in its bearings and only the range needs to be worked at which can be done off board. There were times when the height component too had to be calculated separately and automation of this much technology is not difficult.

3) I don’t deny that F-35 too can share information which is how it is ultimately going to be. As I said PAKFA or Su-30MKI or Rafale need not be silent at all. The silence is merely because the X band radar is not as useful and not because Stealth is a method of fighting with these aircrafts. All aspect stealth is American contribution to the world. The world never believed in it and that is why the world has take only the relevant portion of shaping and RAMs for a limited frontal stealth which will be used only in the attack modes, not in hunter modes.




Don’t look like big kill boxes if you go by, what the professionals are discussing among themselves (refer Dr. Igor Sutyagin in RUSI conference, linked above)




Which is backed by extant technology. Nobody begrudges S-200 or Dvinas or even early generation Patriots.
I'm very pleased to read you....
... but please, make separate answers pleaaaaassssseeeee !!!!
 

StealthFlanker

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F-35 can be played down even without the A-4. :D

F-16 was the F-16D version with heavy loads.
:pound: You think the test with F-16D was to see who win ? , no my dear , it was a flight control at high AoA test , the F-16 was used as a reference point for F-35 to maneuver again


One factor that significantly reduced the F-35 potential in the test was the anti spin logic of FCS


Once the pilot get used to the aircraft and the FCS was fixed , it is a completely different story
https://theaviationist.com/2016/03/...g-in-the-f-35-a-jsf-pilot-first-hand-account/




Nothing like a Rafale
Get off your high horse , Rafale did lose again F-4 too , which is even more lame :pound:

. As I said the representative threats are already developing to a point where they bring loaded supercruise to their attack plan.
Everything have 2 side , going faster give more energy to missiles but it also mean you are alot easier to be detected by IRST. And just so you know in dogfight they dont supercruise.


F-15E was IIRC not the WVR combat but some interdiction mission.
well you recall wrong then . And i already posted link where pilot ranked a 7G limited F-35 higher than F-15E in dogfight.

And the F-15E did not come in with AWACS as they are usually expected and designed to operate
Where is the source that said they didnt used AWACs in F-35 exercise (Green flag and Red flag ) or you making thing up again ?

and don’t have IRSTs.
F-15E can carry Sniper-XR , which is not that different from the IRST on Sukhoi or Rafale nose apart from the fact that it has much wider FoV

So the X-band radar failed to detect. Big deal! Is that the one you are talking about?
The APG-63v3 ( among the biggest and most power fighter radar till date ) and Sniper-XR failed to detect F-35

Also I don’t understand how that education about G load and TWR is relevant.
It is relevant because you clearly still think that a higher stressed g limit mean a more agile aircraft and that T/W ratio is somehow a static value

I mentioned the structural limits for Rafale (11g) only to show that as well as the structural margin of safety to do whatever it wishes to
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Actually where is the evidence that Rafale structure limit is 11 G ? did you got that from Picard again ? :pound:, FYI , just because the pilots did pulled 11G before and the aircraft remain intact , that doesnt mean 11G is the structure limit of the aircraft , when they say for example the F-16 is a 9G aircraft it doesnt mean the aircraft will break when you pull 10 or 11G either , there is always a safety and maintenance margin , in fact while the F-14 is only a 6.5G limit aircraft according to flight manual , and Iran pilot did pulled 11G and still return to base safety ,.The actual ultimate structure G limit is a function of fatigue-life-history and gross-weight. The more fatigue, the sooner the break-up threshold is reached.Military airplanes are usually built with that in anticipation, so that the mathematical "ultimate" figure (1.5x limit-load) is nowhere near the actual ultimate figure - except maybe for an aircraft close to it's design lifte-time.
Nevertheless , the structure G limit play very slight role when you want to compare aircraft agility, a pilot care about instantaneous and sustained turn rate instead. If you want to prove that Rafale is alot more maneuver than F-35 then you will need something called the E-M graph , which obviously still classified at the moment. Alternatively ,we can try to compare their air show performance :
This is F-35 in airshow
it finished a 180 degrees turn in 7 seconds ( From 2:44-2:51) that equal to average turn rate of 25 -26 degrees/second , and F-35 is limited to 7G at the moment. A higher turn rate is considered dominating if the different is around 2 degrees/second or more. If Rafale is so much more agile than F-35 like the fanboy want to believe ,then where is the video of it performing a turn with turn rate of 40 degrees/second or more ? In fact i cant even find video of Rafale turning at 25 degrees/second.

Rafale has the bigger wing,
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bigger wing isnt neccesary a good thing, it will cause more drag at positive AoA , and for your information compare wingloading of aircraft with different wing shape and body shape is irrelevance , why ? because they will have different lift coefficient , ever wonder why F-16 can turn quicker than F-4 despite higher wing loading ? :rofl:

better TWR
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Only if you loaded them with equal percentage of fuel, which will not happen in reality given the fact that F-35 on internal fuel can fly as far as an Rafale with few external fuel tank, if they was engaged on the way to target the rafale will eject EFTs and left with 100 % internal fuel while F-35 doesnt carry fuel anything externally so it already left with less than 100% internal fuel at that point (likely only 50%)
And secondly , as already explained before , aircraft engine thrust is not a constant value , it change with altitude and speed , and at very different rate depending on the inlet and engine design so you cant used the static engine thrust value to compare dynamic T/W ratio


I actually don’t mind it because I have come to accept that F-35 is a Strike fighter masquerading as an air superiority platform and the fanboys imagining air dominance capabilities.
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No, you think F-35 is a strike aircraft because that what you read on some internet forum and magazine.

Also you tend to give a lot of gratuitous theoretical education. Thanks for that effort but I am quoting facts. Mostly admitted facts. And I know which side to err on when faced with a choice between theory and facts.
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No ,you quote half-truth and speculation, coupled with your lack of understanding in both aerodynamic and electromagnetic , you gave pretty laughable assumption and opinion. And yes , i did give a lot of theory educations , why ? because i can see that you lack understanding of even the most basics facts ,all you seem to know is some technical sounding words but that it, with that sort of knowledges you can wow some forum fanboy but not me , sorry.

For Example what do you want to say with the above? That if the F-35 faces off with say an F-16D in real world then the F-16D must first come with disabilities that will change its combat characterstics to a level that F-35 can manage?
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what i want to say is it is nonsense to compare T/W and wingloading with same fuel load percentages if the combat radius of the 2 fighters is grossly different and i already explained the reason why ( the aircraft with shorter combat radius will end up with higher fuel percentage if 2 aircraft done the same mission )

F-35 could have chosen to go with lesser fuel to the tests, if it needed better TWR instead of asking the F-16D to load up with extra load that the F-16D did not need at all for the WVR combat.
Or is it that the F-35 would not have fared any better despite dropping fuel load for a WVR test and the only option left was to load up the F-16D. Is it that the F-35 must load up on fuel because after all that is what it is made for
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As already explained , the test was a flight control software ,not a dogfight to see who win like Reg flag exercise. And the purpose of the external fuel tank is to give the F-16 more time on the air to match the F-35. They can alternatively reduce the fuel load of the F-35 but that will just mean they have less testing time.


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And why must the F-35 load up so much fuel – because it is a known and admitted fact (before some house committee) that F-35 fuel burn is nearly 60% higher than that of F-16C. End result of trying too much
..
It is no doubt that F-135 consume more fuel than F-110 and F-100 , but 60% more fuel ? i dont think so , if it is a fact then you should be able to post a link to support that fact , where is the link ?


They dropped 2 tons of weight and added probably 10% extra thrust.
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2 tons more than the weight of 4 JSOW , and for someone who like to talk about T/W you seem to convinently forgot that P-42 T/W is nearly 2, and it have avriable intake too

You do the same to Rafale it will work nearabout. Do that to F-22 and it will most likely exceed all of them.
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I dont care if a strongly modified Rafale or F-22 without any electronic equipments, radar and different engines can come close to P-42, what i care is that you said performance of normal Rafale is close to P-42 , well no it isnt , not even in your wildest dream.

But F-35 even with similar changes will not. F-35 is a fat flying pig.
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So you cant come up with any calculation or links to support your opinions rather than some fanboy phrases ?


Would not the F-35 be a real super-cruiser already if it could reach 1.2 mach on dry thrust alone?
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English Electric Lightning and F-16 can both reach mach 1.1 on dry thrust alone still they are not called supercruiser .

Why would then the Lockheed official talk about 150nm supercruise limit? Why not just say that the full range in super-cruise is X km?
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because no onefly supersonic from the airport to enemy destination unless you fly something like SR-71 or Mig-31, the range will be reduced significantly because TSFC will increase with speed whether you used your afterburner or not ,.That not to say that supercruise doesnt save fuel compared to afterburner but it still consumed a large amount of fuel compared to subsonic cruise .Even the F-22plannedd combat radius only included 100 nm of supercruise.



I had warned you not to concentrated too much on the strobe which is meant for display purpose only. Still you are stuck with a display functionality.
Ok bhailog you decide.
Given that the Northrop claim is that the strobe is accurate to at least the Subsector level location of a Jammer, so the only thing missing would be the range. The subsectors within a Sector search were allocated by the AWACS itself.
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Iam not stuck with display function, and no you are not just missing just range , you are also missing heading , velocity of target , and missing range is a big problem if you want to attack something ( whether something is 10 km aways , 50 km aways or 300 km aways make a huge different) , in fact there are jamming techniques that the only purpose of it is to deceive the radar in term of range ( RGPO )

Further given that Northrop also claims that only the radar transmitter is shut down and only towards that particular sub-sector where a Pelena-1 equivalent may be
.
what ????? you think that the radar will only be affected when it is directedly look at the jammer ? ( ever heard about sides lobes jamming ? ) and where did Northrop stated that Radar transmitter will only turn off at the sub sector that have the jammer ?

(MALD-J is irrelevant).
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No it isnt , jamming is always related to signal-noise ratio , even the smallest jammer can jam the most powerful radar if either the radar is far enough or target RCS is small enough

Further given that all receivers work full time (no exemption even for the jammer subsector).
Now in order to get the range information would it be too difficult to:
1) have that sub-sector searched by an X-band radar on the escorting fighters (mind you all types of sensors already have their own boresight line of sight fully stabilized and quantified); or
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and what make you think the fighter radar cannot be jammed ? given the fact that they are weaker than AWACS radar and actually more vulnerable to stealth shape ?

2) to generate an artificial aperture by keeping track of that subsector over time (if there is no fighter escort available).
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Synthetic aperture help improve resolution , especially again stationary target ( as used in SAR ) it doesnt help to look through jamming. Obviously, if you keep transmitting (aka increase dwell time ) then you can increase signal-noise ratio to see through jamming , but only to a certain point until your radar cannot determine range due to range ambiguous (no delay between pulse to measuare range anymore )

Keeping track of Jammer bearings is also mentioned with the Vostok-E (see image below, that you asked for). Does that also imply that the Vostok-E has also deteriorated into a Radar Warning receiver?
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as said before ,in passive jamming tracking mode , you lack information about range ,velocity ,heading , altitude of target to generate a firing solution for your SAM or AAM, the only information you have is angular direction so yes in that case you literally function like a RWR, nothing special , ASQ-213 , ALR-69 , ALR-218..etc can all track jammer like that





How does it matter if the jammed AWACS is not able to range one solitary jammer or anything flying under the jammer’s cover when the current scenario is of:
1) abundance of sensors (IR/EO and Low Bands) and
2) every single fighter in a group with its GPS coordinates known and
3) each with its own boresight known and
4) an AWACS level processing power available at multiple points, in air or on ground.
well what make you think there is only one jammer in that case ? if you have a bunch of AWACs and fighters then what stop your enemy from having a bunch of stand off and stand in jammer to cover wide range of frequency and disrupt datalink ? ? what make you think your force is the only one that can use tactic.

You have to worry about the day when you don’t even need an AWACS to process the information and the same is readily done by every non-stealthy Su-30MKI or Rafale.Or the day when one or two small stealthy UAVs each with its own IR/EO sensor joins the fight.
The problem with Rafale and Su-30 is that they can easily be seen on radar , especially when they are loaded with a bunch of missiles. Yes linked together they can use triangulation to determine the jammer (MALD-J ) location , but that it , they still dont see the F-35 that was protected by the jammer
Stealth UAV can certainly be a threat , no one deny that


HEY WORLD, PLEASE NOTE @ StealthFlanker IS SMART.
:laugh: nice , you finally said something smart



Duh man! Do you want to make my arguments for me? Will I allow that?
And no, it was only for Bi-static. I specifically mentioned that.
But look closely ASO is monostatic but the with the same source and a bigger isolated receiver of TASO the picture change completely. ASO and ACTAS serve as the lower and upper bounds for what is possible with several different ingredients thrown in. But the Bistatic arrangement clearly shows that there is a component increase due to bistatic arrangement.
No, i already explained to you the towed array have longer range because it is less affected by the ship own noise ,it has nothing to do with multi or bi static arrangement , in fact the purpose of sonar on the ship nose is not to transmit a sound pulse that will be picked up by the towed array , they dont even work at similar frequency range in the first place.
There are 2 problems that will limit the range a sonar inside the surface ship
the first problem is that it cannot see past thermocline , so any submarine that stayed below shadow zone cannot be detected , a towed array could be put at various deep ,so it can see below the shadow zone ,and also taking advantage of convergence zones and surface duct


The second problem is the fact that the ship sonar will also be affected by noise that produced by itself , such as engine sound , sound of the hull passing through the water creating wave, and the sonar inside the ship cannot even look backward because of the noise comes from the propeller


Now you will said that ACTAS have longer range than TASO even though they are both towed sonar array so that must be due to do multi static arrangement. Well , no , similar to electromagnetic propagation through air ,sound propagation is also affected by absorption in the water itself as well as at the surface and bottom. Sonars tend to perform best where the ocean bottom is hard and flat, and worst where it is muddy (or rocky, in which case, you get more scattering than absorption). This absorption is frequency dependent, with highest frequency sounds being absorbed first, and lowest frequency sounds last. The reason why ACTAS have longer range than TASO is because it use low frequencies to minimise absorption effects while TASO operate at medium frequency.


Multistatic will be many many more times better ranged because the reception is not going to be equally bad in all directions.
So now you basically just repeat what i said at the start , multi static arrangement can detect stealth fighter if the receiver is located at the aircraft RCS spike

this is how a multi static system can detect a stealth aircraft , because for normal radar the receiver and transmitter located at one place so the airframe of the stealth aircraft just have to deflect the radar wave away from the source. For a multistatic arrangement the receiver is so far from the transmitter that the deflection wave from the airframe of stealth fighter may still get into the receiver elements

In the case of radars say Nebo VHF, only the transmitter needs to be safe and protected. The receiver could be right under or even behind the F-35. I would work in such a case just like the Barrier-E FSR, only working at much higher peak powers. Barrier-E was designed for detection Spans of about 25-30 km. You can guess what the Nebo-VHF is going to do.
The receiver need to be protected too ,and it needs to be linked to the transmitter otherwise you won't be able to distinguished between jamming signal , clutter and targets , you wont be able to determine target range or velocity without knowing the pulse transmission time (t=0) and pulse frequency



Master ji, thank you for education but what do I do with this gratuitous education now.
“noise of the ship”! Aapko kanhi direction of motion dikh raha hai picture mein. Atlas Electronik people were careful enough to have metioned that the diagram is not not to scale but they forgot to mention whether the ship is producing noise or not?
It is obvious that when reasonable people make diagrams to show comparisons they do just that and go on and on about unrelated matters.
:pound::pound::pound::pound: unrelated matter ? really :pound::pound::pound: you think the self noise is unrelated matter for a sonar ? :pound::pound::pound:



And in normal operating conditions is that difficult?
Yes it is , spreading your force over a very wide area to the point that they can hardly support each other is not a good idea at all , and not easy to do either.


Nothing theoretically speaking, except may be a bunch of better armed, better informed, fighters like Sukhois and Rafales with much better fighting capabilities.
:pound:You forgot to mentioned that these Rafale and sukhoi cannot get a firing solution again F-35 so they are nothing more than prey in this case

With an AWACS around you can simply forget that an F-35 would get to approach even 300 km towards the AWACS.
And how you gonna stop that ?

BTW is there an internally carried Anti-Radiation Missile also in the works for F-35?
Yes , work is on the way for internal AGM-88E


This says a 30 degree broadside all right but not about +-30 for a total of 60 degrees or +-15 for a total of 30. IIRC the F-35 is LO in the frontal sector right upto +-70 degrees.
It is a matter of where the spike located 30 degrees board side is a total of 60 degrees , given that it is an AWACs that fairly reasonable.

Anyhow this itself constitutes an interesting input. If the Typhoons did in fact for a multistatic arrangement with a singular AWACS, it implies that the Typhoons have the receivers for the S-Band transmitted energy.

The X band transmission by Typhoons would be practically useless in most cases for a multistatic arrangemen
No , it is simply that AWACs pass down the information to Eurofighter by datalink , nothing about multi static here :hail:why the hell are you so upset with multistatic arrangement ? , the point when i posted this is to tell you where the high RCS spike likely located

Which leaves us with the quaint question is the L-Band antenna on PAKFA an IFF really. There is a lot of Cows being denounced as Goats.
Nope , according to official information , it is simply an IFF and ECM system



Or is it that a simultaneous claim of use of multistatic arrangement, AWACS and Tyhoons are suggestive of even IRST &/or S-Band mixed triangulation.
In any case this states that the 4 Typhoons were successful in intercepting 8 F-35 and that some sort of multistatic arrangement was actually used which basically supports the claims being made about the approach Russians have taken.
let not forget the detail , it is 4 Typhoon in interceptor configuration intercept 8 F-35 in air to ground configuration , and the F-35 only equiped with 2000 lbs JDAM instead of SDB which have much longer range. And eventhough Typhoon have IRST too , it still has to rely on AWACs being stationed on a certain angle in respect to F-35 flight path



No, the Eurofighter official (Craig Penrice, a Typhoon pilot and marketing adviser) says and suggests nothing about the spike being at the 30 degree dogleg. ‘Can be defeated by’ cannot be read as that being the only approach, nor can it be read as being the most efficient approach.
So you think that Eurofighter official will not used the most optimized situation to advertise their aircraft ?:pound:

What I am noticing is that you don’t actually read much of anything. You just skim through things without even focusing, looking out only for things that seemingly support your pre-conceived notions..
And i think you are doing that too , the only different is that you lack basics understanding and you dont even seem to try to learn at all.


No, you are trivializing the whole concept.
People are trying to develop multistatic SAR, ISAR and range increases, netted radars, GPS radars and you are stuck with the 30 degree broadside argument that too without providing a real study. I have waited enough for your study. I doubt its very existence now.
All you have given is a sparsely backed claim by a Eurofighter marketing official who does not even refer to a study about multistatics. In fact the only mention of study in the flightglobal report you provide is a modeling of the possible interceptions.
No i dont trivializing anything , it doesnt matter what radar system you used , they have to obey physics, and if they obey physics then they will have limitation. You are simply acting as if multi static arrangement is some sort of godly radar that have no limitation and can detect stealth aircraft from any distance well that not how physics work. As i already explained like a thousands times before and you still dont understand ( or pretend not to ) and still dont read up about it. The only reason multistatic arrangement can sometimes see stealth aircraft from longer distance than mono static arrangement is because the receivers sometimes located at a direction where the RCS scattering is high ( or by your own words , signal is not equally weak in all direction ) . Multi static arrangement doesnt magically give your aircraft ability to see targets hundreds km aways regardless of their RCS. It isnt immune to jamming either.
I already posted a picture of a simulated RCS scattering of F-35 shape ( because the capabilities RAM and RAS on F-35 is still classified ), and the links about Eurofighters simulation , they are to show you that the RCS spike isnot at the frontal direction ( to be honest anyone with even a bit of common sense will know that designer are not going to design stealth aircraft with high spike at the frontal or only 3-4 degrees of side), the point was not that they use multi static arrangement, the point is that because the high RCS spike is very far from the nose , your receivers and transmitters in your multi static arrangement need to be located at long distance from each others



Please either provide the study itself or accept that the information is not enough.
:pound::pound: so where is your study to prove that multistatic arrangement will absolutely works again F-35 ?







Bhailog now consider this, the range for a monostatic radar is a root 4 function. The range for a bi-static system (non-FSR) is a root 2 function
No it isnt that simple , the only thing that is different for bi static from mon static is that the receiver isnt in the same place as the transmitter anymore , so now instead of using only the distance from transmitter to target to put in radar equation , you need to include distance to from receiver to target in the formula as well.So even though , there is only root 2 , you actually ended up with 2 R value so the final value isnt that much different The only case that it truely come down to a root 2 is if your receiver is literally at the same location as the target ( which is rather impossible to say the least ).







. Obviously as the PAKFAs race towards the F-35 receiving the AWACS-radar-returns the reflect signal has to travel less and less. F-35 must now decide to either enter the merge with obvious disadvantages or to abort mission and return.
So what would stop the F-35 from launching missiles at the PAK-FA , Rafale in this case ? ? and btw you still havent answered my question last time , if stealth directional datalink doesnt work and can easily be detected then how can your Rafale , PAK-FA take advantages of multistatic arrangement ? :pound::pound::pound:

At this time if the F-35 decides to return they will expose their 190 KN tail and that will be seen and triangulated on the IRST at more than 90 km, with the superior speed of PAKFA still on its tail.
:pound: so you dont want to use Rafale no more ? changed to PAK-FA now ?
:pound:If PAK-FA close in with such high supersonic speed then it will show up quite clear on EOTS and DAS too , so what will stop F-35 from attacking the PAK-FA force ? :pound:



Stated to be something like this:
Actually the only way for the Su-35 , Rafale to maintained the angle is if the F-35 doesnt turn , there is nothing to stop the F-35 from seperate into 2 force , one facing the AWACs , the others facing the Sukhoi , Rafale. :pound:Once the AWACs is down , it over. The simulation did by Eurofight also said nothing about possible jamming from F-35 force :pound: And honestly you grossly optimistic about the speed different between F-35 and Rafale here


Here are two a links for root 4 and root 2 calculations which will show how the radar range is affected due to this factor for any given radar equation:
http://www.squarerootcalculator.co/
http://www.calculatorsoup.com/calculators/algebra/fourthroots.php
Note :To calculate the radar range between monostatic and bistatic arrangement the number that is to be ultimately rooted off is the going to be the same, presuming all things being equal. Range difference can arise due to other factors too but the biggest factor is only this singular factor. And mind you the ranges they mention in the brochures normally is the monostatic range.
:pound::pound: Did you forgot that there is 2 different R factors in bi static arrangement ? :pound::pound::pound: No my dear , the range isnt square up :pound:



you are reading things in a very different manner from the way I am. I do not deny that angular separation is needed and helpful in some circumstances, but then you put both legs of the triangle at same distances. Angular separation can still be maintained should you need it, even if one side of the triangle is shorter (fighters) than the other (AWACS). And with AWACS or IRST, that is easy to achieve.
Yes , one leg can be shorter to target than the other , but the problem is you cant just teleport your fighter there right next to the F-35 or close to it, before the fight start you dont know where the F-35 will come from you already put your receiver and transmitter at a certain distance from each other that that will form adequate angle with target. For example in your picture , you cannot put your aircraft at the Red arrow from the start , because you dont know where exactly F-35 will come from before the fight , you can only start from Green arrow, which mean your fighters and AWACs would be quite far from each other ( or your receiver and transmitter in multi static arrangement have to be far from each other if you like) Use simple math and you will see how far they need to be from each others to detect an F-35 from 200 -300 km. And now think , what if F-35 didnt come from the top in the picture ? ? would your Rafale run quick enough to save the AWACs if F-35 come from the right ? would they be able to defense them selves if F-35 come from the left ?
 

BON PLAN

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:pound: You think the test with F-16D was to see who win ? , no my dear , it was a flight control at high AoA test , the F-16 was used as a reference point for F-35 to maneuver again
In your dream.... In this case why not simply saying that from the USAF officials?
 

StealthFlanker

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VHF+S-bands will be able to provide a good kill box. Here is what a professional Dr. Igor Sutyagin has said in a conference of professionals, published with no professional counters till date:
:pound::pound:Oh dear , i already told you before , you really need to understand the basic before cited some advertised number . Read carefully what they said "60 meters for distance measurement " what does it mean ? it mean the range resolution of the system is 60 meters . So what determine the range resolution ? it is the pulse width , shorter your pulse is , the better you will be able to determine range


But what is the problem with short pulse ? with same average power the shorter the pulse the less energy you transmit , less energy mean less range , low-frequency radar already have low gain thus their energy is less concentrated , now you wanna use short pulse too how far do you plan to detect the F-35 ? :pound: . And the problem with low-frequency radar is not only their range resolution but their angular resolution :pound:, range resolution can be improved easily by using shorter pulse , angular resolution ? not so simple :pound:other than getting a massive aperture , there isnt much you can do






If the above is true then the F-35 could be in very real danger even for its primary and only role of Strike.
Nice try included some of your fanboy opinion as if it was hard fact :pound:


Unless the guidance is command guidance+INS. Off course the fighter should still know where to lob the semi active AAM but the CW mode can come up only at the last 9/10 pings probably last 4/5 km at 3+ mach. Or if the Active Seeker itself comes on at the very last moment only to acquire the target, travelling almost all the time as a simple command guided rocket.
:pound:When i said 4-5 km , i mean if target is only 4-5 km from you then you can launch your missiles without knowing range and even velocity , but if target is 50-100 km km aways , you need to know range ,altitude , heading and velocity otherwise your missiles will never reach target , all BVR missiles fly a ballistic curves with lead intercept to reach long range , all these are not possible without vital infor that i listed above :pound: , they dont just divided radar into several mode for fun you know :pound:

So that will leave very little time to react. And similarly will be case with F-35 trying to avoid SAGG of S-400 by flying low where the EOTS capabilities themselves will have to be sacrificed by F-35.
F-35 dont need to use NOE to avoid radar , that what fighter without VLO characteristics such as rafale do

.
F-35 or MALD-J will have difficulty even jamming because nothing is being transmitted in the first place in X-Band or Ka-band. And during these final moments the X-Band radar of the S-400 battery, with much more power at its disposal, will also light up for the final kill. Each part of the system falling in line just when its needed.
:pound:what make you think F-35 can only detect signal and jam in X or Ka band ? :pound:what stop F-35 from stay at long distance and loft these JSM , JSOW-ER or SPEAR at S-400 battery ? it not like the S-400 is stealthy isnt it

flying higher will bring the IRST of Sukhoi/Rafale into play given the big F-135 engines and clearer weather.
Same problem again IRST need to rely on LRF for range and velocity measurement , and LRF isnt so high , and btw engine thrust isnot directly proportional to the heat give out :pound:, It is unlikely that a high bypass engine like the F-135 would be hotter than low bypass engine like Snecma M88 .


After reflection it will travel. .
what reflection ? are you taking about TDOA to determine range in completely passive arrangement ( you have no transmitter on your side and rely on enemy radar pulse ) or multistatic radar arrangement ( where you have at least 1 transmitter ) ?

In any case the track beam need not even figure in all this because there is no need to use TDOA for triangulation. Only angles are needed which for systems equipped with boresight and gimbaled LOS is known in advance
triangulation and TDOA are 2 different methods.




Yes and the receivers too can be a chain of several small Ka band antenna.
It doesnt matter if your receiver is also Ka band , the advantage of Ka band datalink is that it is very directional and it have very high attenuation , so unless your receiver stayed between 2 F-35 communicate with each other , you wont be able to detect it, that the point.


The TDOA and FDOA as you rightly pointed out would normally need same source (transmitted or reflected). With encoding of identification signals even a singular source would not be needed and all receivers would be receiving many different reflected waves from many different targets illuminated by many different transmitters and no transmitter truly jam-able, i.
It doesnt work like that , without the link with the transmitter you wont be able to determine distance to target , it's heading , it's speed , its altitude. If you use many transmitters and absolute no data link between each transmitter and each receiver then how can you even used triangulation , FDOA or TDOA ??

Better to use this tech development path then to go all stealth.
what make you think a stealth aircraft cannot take advantages of jamming ? if anything stealth make jamming much easier and effective for the platform

If a receiver at all instances knows for every target the TDOA and FDOA and knows this from multiple different transmitters with accurate PNT information available easily, .
TDOA , FDOA, triangulation all required you to link and communicate between different receivers , you cannot do that with only 1 receiver , so your rafale have to talk to each other , hence my point
"if datalink is so easy to detect then how can your Rafale use TDOA or triangulation for passive ranging then ? how do you think multi static arrangement work ??"


what stops the network from even imaging a target.
generally resolution cell of the radar

But why do you invoke TDOA at all for multistatic radar. I just mentioned TDOA in the context of Arty Sound Ranging and that part is done. Mere triangulation is enough for taking on F-35. Only range information is difficult to get and that too only in higher bands and that too only with the one-on-one merges. For the first detection you will require 2 platforms but for all (which could be hundreds) the later detections, you will get as many ranges from as many angles as there are platforms to calculate angles. The nature of the triangle itself dictates that. The Typhoons probably just did it going by your link, foiling 85% of the F-35 strike missions.
If you use TDOA or Triangulation or FDOA , you all need a link between receiver aka the link between these rafale , so if you think stealth datalink doesnt work then your silent multi static arrangement wont work either .
And i was talking about TDOA ,triangulation for radar warning receiver , you are talking about TDOA and triangulation for multi static radar.
In the case of TDOA ,triangulation for radar warning receiver , my argument was that if you rely on RWR and TDOA or triangulation between multiple Rafale to get a firing solution again F-35 , then nothing will stop a single F-35 from transmitting and share information with it's formation through stealth datalink MADL. You go on and said that stealth datalink doesnt work and can easily be detected. That why i said , if you think stealth datalink is very easily to be detected then how do you think your Rafale, PAK-FA can rely on TDOA or triangulation and silently get a lock on F-35 ( given such techniques require sharing information between multiple platforms )

In the case of TDOA , triangulation for multistatic radar , the problem has always been getting enough seperation between receiver and transmitter so that your receiver can be located at the direction where F-35 have a high RCS value


Master ji abhi to IRST apertures have not even started evolving. What will the F-35 or even F-22 do, once they do. And then what will happen when these big apertures also sport scanning capabilities.
IRST can already scan , and no matter how they envoled , if they are still in IR wavelength then they still have certain limitation due to physics
And IRST is not imprevious to damage or jamming either




Besides you seem to be ok with omnidirectional datalinking being effective, so it should be very very effective in guiding AAMs too. Should it not?
Yes



I don’t care much for Spectra and MALD-J cannot jam AWACS.
MALD-J will off course work against Active seeker heads. That is its main use. It probably may also have X-band capabilities because the Americans are ahead of all in this kind of dual band arrays. So MALD-J may also work against FCR of fighters. But this will affect only those air forces who are relying still on improving their X-band FCR to be able to work against LO targets like the Swedes. For those relying on MIMO multiband radars and IRST this will have nearly no use.
Again , you still dont understand the relationship between jamming , RCS and signal-noise ratio , you really need to read up on that













The Americans are thinking is that they should spoil the end game for all SAMs/AAMs hence their focus on DIRCM and Standin jamming. Essentially they have already conceded that jamming at long distances is not useful or practicable. While SAMs and AAMs will evolve again to take this into account there may be entirely new technologies that will facilitate this evolution.
That is absolute nonsense , EA-18G and NGJ are both for standoff jamming







The difference FOPEN designers were making was about man made decoys (including chaff) and just leaves, trees, rain, hail and bad weather – while compared in the X band and UHF/VHF.
Nope , it still not easier to make decoys in X band , if anything VHF and UHF band actually effected more by weather due to ducting effect


I personally don’t mind chaff for lower bands either. Actually I don’t mind any jamming at all, speaking from an defenders perspective. Jamming of any kind implies there is something interesting to be found.
The problem is where exactly and how can you engage it

In fact the difference is stark even if the systems are from the same countries. American have for long operated VHF long range sensors for space applications. There X band ICBM watcher however failed. Both being as of today.
The VHF sensor is always for early warning , they dont use it for FCR , main FCR for ICBM such as THAAD and SPY-1 still in high frequency instead of VHF or UHF

Who is challenging you on your radar burn throughs?
Do I look like I care for that?
Yes you did challenged me when you keep on saying that MALD-J cannot jam AWACs because it look small , and iam sure you dont care because you dont actually understand why did i talk about burn through and signal-noise ratio :pound:as i said before , read , try to learn before you comments
And besides it is you who is being unfair and doubting Sepctra even though it carries the same tech. (an old tech.) for radar waveform cancellations only at a lesser distance (which BTW also implies smaller formfactors for Spectra hardware).
:pound:How am i being unfair ? it you who keep insisting that MALD-J cant jam low frequency , but have no problem believing that Spectra can operate from 1 Hz to 100 Ghz :pound:oh and FYI , jamming at closer distance is actually harder


Besides it is you who does not want to acknowledge that for bistatic arrangements the range increases merely because the waves don’t have to travel back as far and this return path distance could be closing in at Mach 2 or 3+.
Do you event read what you wrote ? :pound: so the range increase because the wave doesnt travel back as far ? what ? are we talking about range to the receiver or range to transmitter here ? , and how do you know what direction the enemy is to close in before you even detect them ?

While for ‘Jamming vs. Jamming burn through’ it is a simpler issue because both transmissions are towards each other.
go learn how RCS affect burnthrough distance

Which is also why the French are claiming that they have spent close to 25% of Rafale development cost in making the Spectra which will analyses the radar from the first transmission itself and will have a big library of all waveforms that the F-35 cannot change easily. .
Frequency hoping and PRF jittering are among the easiest things to change :pound::pound::pound: especially for modern radar with their wide bandwidth, and for active cancellation to work you need to know exact frequency and phase of the radar pulse to produce "cancelling pulse " , good luck doing that to something that can literally change frequency randomly with every pulse :pound:



You will basically be detected long long before you can even bring your MALD-J into consideration, which in any case cannot jam any sensors that are not already discounted.
Discounted according to who ? you ?
You do get redundancy by MALD-J but what is the point if you can be seen all of EM spectrum except the X-band.
I already explained to you that low frequency is not magic , stealth aircraft dont suddently have RCS of thounsand dBsm at low frequency , go back previous page and read FFS
http://defenceforumindia.com/forum/threads/know-your-rafale.32861/page-224

So you highness allows for the IFF to retain its importance without answering the main question as to why would the Russians need their interrogators to be this big when the whole world is doing it differently? Detection and targeting of a LO target is a challenge but how is interrogation a challenge?
Bigger aperture = higher gain = longer range = able to do IFF at longer distance = able to engage sooner while still obey ROE , pretty important for stealth aircraft if you ask me ( but ofcourse fan boy dont care about IFF )



( abit busy now so i will answear the rest later )
 

BON PLAN

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F-15E can carry Sniper-XR , which is not that different from the IRST on Sukhoi or Rafale nose apart from the fact that it has much wider FoV
can carry, yes. But in this training it wasn't used. Sniper is mainly (not to say only) used for AtoG use.
 

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