EF in Egypt is all but sure.After Qatar, it seems Egypt too will be operating EF2000 and Rafale combo.
EF in Egypt is all but sure.After Qatar, it seems Egypt too will be operating EF2000 and Rafale combo.
Why? because the nose is slighly bigger?Typhoon AESA will be superior to RBE-2 AESA.
German, Spanish Eurofighters will receive the world’s most capable fighter jet radarBecause it's >1.5x bigger precisely. That gives it more than a 3-fold advantage on the top-line of the radar equation.
You do suffer from confirmation bias don't you. The number is around 1,500, which complies with 1,000+, 1,422 rings a bell. The Rafale only has 898, it's a tiny radar.
1000+ T/R Modules: same claim as RBE2 Rafale Radar!
More than 200 Km detection Range same claim than RBE2 Rafale Radar at initial deployement !!
Perhaps there is not enough power to add more T/R or perhaps it's too hard to extract the heat on a repositioner ????
Developed over 10 years means 10 years late perhaps, who know?
I stand by the fact that Airbus claims 1000+ T/R and Thales also claims 1000+ T/R so for me it is likely that the number of T/R modules of the two radars is equivalent. Otherwise I would not understand that the range of the E-Captor is only 200 km.You do suffer from confirmation bias don't you. The number is around 1,500, which complies with 1,000+, 1,422 rings a bell. The Rafale only has 898, it's a tiny radar.
While TRM count does help but it is not everything.....first generation AESA with 1000 TRM count can be outgunned by 2nd or 3rd generation AESA with far less TRM. radar range is factor of many things.You do suffer from confirmation bias don't you. The number is around 1,500, which complies with 1,000+, 1,422 rings a bell. The Rafale only has 898, it's a tiny radar.
You're looking at a mock-up, not the real thing. Basically a tin plate.While TRM count does help but it is not everything.....first generation AESA with 1000 TRM count can be outgunned by 2nd or 3rd generation AESA with far less TRM. radar range is factor of many things.
•Captor E AESA
View attachment 16637
View attachment 16636
• RBE-2 AESA
View attachment 16638
there is massive difference between both of them. Captor E AESA use slotted waveguide Array while RBE 2 AESA use flared notch radiating element. Later offering far higher bandwidth, higher directivity hence increased range despite less TRM and tiny size.
View attachment 16639
@Picdelamirand-oil
What the heck does 1000+ mean? 1000 plus what? It's like 'more than 200km detection range'. Against what RCS, what does 'more than' mean, how much more. Other sources say it can detect an F-35 at 60km.I stand by the fact that Airbus claims 1000+ T/R and Thales also claims 1000+ T/R so for me it is likely that the number of T/R modules of the two radars is equivalent. Otherwise I would not understand that the range of the E-Captor is only 200 km.
As long as the radar was a project, Airbus could tell anything, but now that the radar is well defined they are obliged to get closer to the truth because otherwise future customers will ask themselves questions by discovering the true characteristics of the Radar.
Surprisingly when you're told the same kind of thing about the Rafale's performance you don't want to hear it.What the heck does 1000+ mean? 1000 plus what? It's like 'more than 200km detection range'. Against what RCS, what does 'more than' mean, how much more. Other sources say it can detect an F-35 at 60km.
F-35: a game changer in modern warfare
www.koreatimes.co.kr
Because we know for an absolute fact that the Rafale's radar aperture area is smaller and that tends to determine detection performance, just like we know that a variable flow ducted rocket provides greater range than a solid rocket motor. It's commonsense.Surprisingly when you're told the same kind of thing about the Rafale's performance you don't want to hear it.
Why should we consider that the antenna on the photograph of the E Captor is that of a moke up if you don't want to consider that the antenna of the RBE2 on the photograph is that of a prototype which does not have the same number of T/R as the standard equipment.?
Because we know for an absolute fact that the Rafale's radar aperture area is smaller and that tends to determine detection performance, just like we know that a variable flow ducted rocket provides greater range than a solid rocket motor. It's commonsense.
Yes you'r right the supplier is UMS same technology for T/R module. But the antenna is different and if you'r able to extract more heat you are able to increase the power.I thought Europeans used the same antenna tech in order to reduce costs. So I suppose Rafale, Gripen and Typhoon have the same supplier for the T/R modules. Or am I missing something?
Yes you'r right the supplier is UMS same technology for T/R module. But the antenna is different and if you'r able to extract more heat you are able to increase the power.
We don't know that at all, it's just your assertion. What we do know is that Captor-E spent much longer in development than RBE-2 AA.But we also know for a fact that Typhoon's technology is crap and this proves that they will never be able to tune their radar to get all the potential performance out of it and moreover they won't have enough electrical power available to put all the T/R modules that the size of the antenna allows nor the ability to extract the heat optimally due to notorious incompetence.
As I proved that it is possible to make an X-band antenna with more than 1000 T/R of the size compatible with the nose of the Rafale, the nonsense of your free assertions is of the same order as that of my own assertions above.
MMRCA 2.0 - Updates and Discussions
Yesh, you don't know basic facts and math. Forget replying to me. Why don't you enlighten me with your superior facts and math. I would like to clarify that 400 km radar range is in narrow FOV for F 22..... Between 200- 250km in case of Rafale.www.strategicfront.org
As it is just your assertion that RBE2 AESA is 892 T/R.We don't know that at all, it's just your assertion.
What we do know is that Captor-E spent much longer in development than RBE-2 AA.
The argument is completely ridiculous, the power of a reactor is never a limiting factor in power generation, the gap between the two is too large. And your E Captor will be integrated on tranche 3 and on Tranche 2 so it has to fit with the least interesting specifications.What we also know is that Tranche 3s were made specifically with more cooling and that EJ200s are more powerful than M88s and can hence generate more electrical power.
But we also know that Jaguar BMW and Citroen do not develop AESA antenna.What we also know is that Jaguars are made in the UK and BMWs in Germany, whereas Citroens are made in France.
It's not so easy to make a good AESA antenna : Same T/R modules were available to the French and the British at the same time and the British are 10 years late. The software is needed but not for the performance we discuss in Forum.It would make more sense to believe the main factor that will create the biggest difference will be software rather than hardware.
Wasn't my assertion, someone else counted them way back.As it is just your assertion that RBE2 AESA is 892 T/R.
Which prouve a lack of competence
The argument is completely ridiculous, the power of a reactor is never a limiting factor in power generation, the gap between the two is too large. And your E Captor will be integrated on tranche 3 and on Tranche 2 so it has to fit with the least interesting specifications.
But we also know that Jaguar BMW and Citroen do not develop AESA antenna.