not stating internal A2A means there may also be external missiles, it says nothing about external tanks,
stating internal fuel OTOH rules out external fuel
Do you think the combat radius for Gripen Ng clearly include 20 times mid air refueling? 😉 Since it clearly didn’t specifically exclude mid-air refuel either
this is how internal configuration looks like when range is an issue
https://www.google.com/search?q=f-22+drop+tanks&client=firefox-b&tbm=isch&tbo=u&source=univ&sa=X&ved=0ahUKEwiH75q2_IbTAhWMKY8KHdrxDksQsAQIGg&biw=1060&bih=466
You wrote “F-22 drop tank”
F-35 internal configuration look like this
http://lmgtfy.com/?t=i&q=F-35+internal+configuration
Eighter way Sukhoi’s range stats would work just fine as a metric.And when we talk about optimized cruise altitude. Its very similar. Its perhaps Special jets like Mig-31 and F-22 that cruise above. All other its the same ballpark. The take-off and climb should also be the same or are you telling me the range are only from a air refuel??
No, iam telling you that the profiles that manufacturers publicised is up to the buyer’s decision. Some buyers will want to know the low altitude strike mission range, some may want to know the high altitude interception mission range. Some may want to know medium altitude SEAD mission range ..etc. They do not want the same thing. So manufacturers donot use the same mission profiles.It is important to remember that they do not really need to convince general public but rather the people in procurement process
Anyone with half a brain understand that Fuel consumption goes through the roof when AB being used.
Yes but not at the same rate for all aircraft.
Why would you NEED to know the combat radious if you KNOW both jets in any comparison, fly at optimum acruise altitude or at deck altitude. With four A2A missiles.
Both jets, launch all missiles at half distance out, or at bingo fuel, then Return to base.
Sukhoi spesify eighter optimal cruise altitude or deck altitude, at M 0.7 cruise speed.
You dont understand what iam trying to say. My point is those figure for combat radius between different manufacturer is not easy to compare because they may include different altitude and different time on afterburner..etc. If you can get a comparison where they both use the same profile, only then it would be a apple to apple comparision. It is also important to note that, combat radius public by Manufacturer are often for buyer to consider their choice. As a result, the chosen mission profiles is pretty much the buyer’s decision
Moreover, include AB time will make a big different especially in case of twin engine aircraft. For example: comparing F-15 to F-16, there is only ~25% increase in fuel consumption while cruising but 174% fuel required for full AB maneuvering
I have looked them up, it’s all in the original message. The combat radius of the F-16C is 675 nmi in the A-G config
F-16I with Conformal fuel tank, 600 gallons tank (unlike 370 gallons tanks, those one are not jestionable ), 4 AAM and 2 GBU-10 can reach 630 nm
It looks like this
You can drop that nonsens right away.
I have questioned this many many many times before, and until this day i have not seen any REAL figures that would explain the F-35A REAL range.Why must it be so freakin hard for LM to file weight and Range figures like this:
http://www.knaapo.ru/products/su-35/
нормальный (2 x РВВ-АЕ + 2 x Р-73Э)
H=0 M=0.7
etc etc etcThe only reason is; it would be kind of revealing in a bad way.
Most manufacturers doesn’t give combat radius in that way. Moreover, the figure you gave also doesn’t reveal much. What are the combat time ? ( time on afterburner) , what are the loiter time …etc.Those certainly affect the combat radius. The profile could be complex too rather at a specific altitude
above all it depends on if there is external fuel tanks included in the estimate, like the above pic does
F-35 has no external fuel tank
And in which altitude flight profile is this done?
To be fair, no idea.Public combat radius rarely include altitude if ever unless you get it from flight manual. But i would assume it is at around 35-40k feet since those seem to be the most optimum for turbofan engine.
As per the latest SAR the revised APB (post baseline) for the JSF put the F-35As combat radius requirement at 690 nautical miles (Objective) and 590 nautical miles (threshold). The current estimate is 625 nm.
It is also depend on specific mission
Not what Halloweene was talking about. He was talking about different modes operating simultaneously,. The APG-81 can’t do that (according to open source material), neither can the RBE2. They use interleaving which is pretty much the same thing to the user- generating a SAR map and track while scan for example, the switch is measured in nanoseconds so I’m not convinced it’s that imperative
Fair enough. But since we know AESA can form multiple beams, i think this is a software problem rather than hardware problem.
I see your point. But if the interleaving mode has such short time delay then what is the point of dividing the array into sub arrays for different tasks ?. You will lose out on accuracy and detection range
Interleaving mode leads to high duty cycle.
Well hint : type NATO MACE Xii and Rafale about S300.
I actually searched that before, Rafale did join MACE XII with F-16A and F-4 but apart from some internet rumor, there isn’t any official information regarding how well it done or the K/D ratio
Sensors? Not so sure (RBE2 AESA more recent than APG e.g.)
While the technology level between them two are up to debate, it is undeniable that APG-81 has much bigger aperture. That will give it quite a bit of advantage in range and resolution compared to RBE-2
Physical division of the antenna is coming (MELBAA programfunded in (2014) that will allow simultaneous allowment of diferent parts of the antenna to different tasks. (nad not switching very rapidly like APG81) for ex
APG-81 can form multiple beam at the same time ( in fact, practically speaking, any AESA can do that because they use seperate T/R modules instead of rely on a single traveling wave tube ,so different part of the aperture can transmit at different frequency )
I am inclined to believe that the better computing power to design stealth airframes has made it so that the jet design has to be less compromising to the shape/aerodynamics of the aircraft but is not necessarily better absolute stealth.
So if they were to make something as stealth as possible, at the expense of aerodynamics and performance, that the aircraft that they come up with, would look more like the F 1117 than the Raptor.
It would be super cool to see someone design the most stealth airframe possible, with all the coating tech applied too. I am a coatings skeptic. Which is why I think the F 1117 might actually be a more practical stealth jet. Because it relies less on coatings and more on the brute force of angles.
KGB is right on this.. A curved shape will never be as predictable as a straight angled edge and will always have reflections to all possible directions which, then have to be handled by RAM.. there is no way around it..
No, F-117 is not the absolute shape for stealth, unless you only care about specular reflection. In reality radar reflection consist of various different kind of reflection. In optical region then specular reflection is more important than traveling wave return, surface scattering but as wavelength get longer relative to aircraft ( Mie or Rayleigh region ) then surface scattering become more and more important.

A curve often has wider specular reflection cone than a full facet, but the benefit is that it can have less surface scattering. One can look at various modern VLO platforms and noiticed that eventhough many of them don’t need agility at all , yet none of them uses full facet design like F-117. Notable examples are B-2 , X-47 their center bodies are actually quite curvy ( even from front aspect ) while there is not a single curve on F-117 design.

On the other hand, a full circular/tube body or nose is very bad for stealth eventhough they have less scattering than a full facet design. The reason is that surface wave will travel the whole circle around in that case . Thus, reflection will be much higher. At the same time they still have wider specular reflection cone


The idea of your YouTube channels is interesting. But if you want more subscribers, video should be shorter. Like around 5-10 minutes top (you can divide your video into several sub video) . Most people would be hesitant to spend 42 minutes watching a video unless it on TV.
Ours are 1.1 meter in length
Probably for very low frequency then
I think we’re back to square 1, unfortunately. The original poster exclaimed this was an L-band AESA, but I assumed he was just exaggerating
Using L band for fire control radar of fighter would be horrible, the aperture would be too small, beamwidth would be massive and you ended up with a very low-resolution radar system
The 1760 module TR count in other documents means that this is not the J-11B AESA, it’s something else, although presumably from these figures it’s likely to be Flanker-sized
where is your 1760 T/R modules number came from ?
the red value i saw in picture is 804, if that isn’t T?R count then what is it ?
At the same time, though, the Chinese media claimed 450 km range on the J-11B AESA, so perhaps it IS L-band and the X-band AESA was discarded, or alternately the L-band achieves 450 km detection against 0 dBsm, but the X-band has an inferior detection range.
Not really, for the same transmitting power ,internal noise and aperture size ,assuming against a fixed RCS value (instead of a fixed target). An X band radar will have longer range than a L band radar. Because wavelength is much shorter so gain is massively bigger. That lead to significantly better directivity while anttenuation would be very small at such frequency.
In reality same target will has different RCS at different frequency but that not what considered in your photo
Heading: Maximum Detection Range vs a RCS 0.1 m^2 target
Figure 4.5 Greatest Discovery Range at Dissimilar Elevations (RCS 0.1m^2)
Column Headers:
Target Elevation (Meters) / Maximum Detection Range In Normal Early Warning Mode (Kilometers) / Maximum View Line Range [???] (kilometers)

It is rather confusing
I can see that detection range increase between look up vs look down but why would there be detection range improved between 6000 and 8000 meters too ? do they give altitude for J-10B in their estimation ?. Maximum view line range probably referred to radar horizon , you can calculate J-10B height from radar horizon and target height but i cant be bothered at the moment
P/s: never mind , it isn’t radar horizon. If radar horizon for target at height of 8000 meters is only 383 km then the radar is basically on the ground
there are many strange values but too strong language barrier
But back to the F-35, so that implies, first, the F-35’s cockpit is so cramped because Lockheed wants to minimize the RCS of the exposed cockpit. Likewise, the F-22, unlike the F-35, can reduce RCS by making the bottom the exposed aspect, so only the edge of the radome would be reflected.
There are transparent RAM though, so the cockpit isn’t exactly exposed. I think the cockpit is quite big though apart from F-35B but that due to lift fan
Thing is, detection range is often cited as 2x tracking range. If you cite APG-81 tracking as 160 km, you get 320 km detection range
Not really that simple.
It depend on what sort of tracking you talking about, like tracking by conical scan or monopulse ?
We should also consider that tracking range of legacy radar often be much shorter than detection range due to PRF limit, higher PRF lead to more radar power on target but also shorter unambiguous range because reflection may come back before new pulse is transmitted. But on newer radar due to pulse compression, they can distingush reflection pulse much easier because the radar would know the compression codes/sequences, so it likely that there are less difference between detection and tracking range
Check the images out
I can’t read Chinese so i don’t understand anything in your photo. Can you translate those words in 2 table to English ?
If iam not wrong the last photo is elements counts ? the 800 T/R modules is quite low for Su-27 size aperture, unless it uses lower frequency than APG-81/77
About the RAM, your posts show around a peak -35 dBsm in the 8 gHz X-band range, so we could be looking at -60 dBsm F-35s and F-22s. Sort of scary stuff, and moreover, the stuff that’s released is unclassified, implying that actual classified RAM could boost F-35 to -70 dBsm in the X-band
I don’t think F-35 can reach -70 dBsm level ( i could be wrong though but still ), the reason being that there are several place that you can’t really put normal RAM on such as antenna ( there are frequency selective surface but we dont know their effectiveness ), RAM on transparent surface like canopy and EOTS window will likely be less efficient than normal RAM. Aspect is important too.
sounds like you know more than you let on, and at the same time, you won’t say anything that’d get you in jail, right?
No.