Since the AWG-9 and Irbis-E radars have nearly identical aperture sizes (0.91 m vs. 0.9 m), and if assuming they operate at the same frequency, their beamwidths should be approximately the same - around 2.3-2.5 degrees.sprstdlyscottsmn wrote: Assuming a 2 degree beam width, the AWG-9 1-bar is a 20x2 scan or 10x1 beams, and is ALSO not very useful unless you are told the general bearing and Altitude of the target. The Irbis-E 10x10 is then 5x5 beams and as such has even less dwell time than the AWG-9 figure shown. Having a 10x10 vs the 20x2 means you are less sensitive to needing to know the altitude but need much more accuracy on the bearing.
The cued search mode of the Irbis-E covers a volume of 100 square degrees, which could correspond to different scan patterns. For example:
A 10° × 10° sector for close-range targets, providing a balanced horizontal and vertical coverage.
A 40° × 2.5° sector for long-range targets, where vertical angular variation is minimal, allowing a wider horizontal search
Either way, a 10 degree cued is well within capability of the RWR. You can increase dwell time by spend more time on volume search. If we assume the Dwell time per beam position to be 0.03 seconds similar as Zaslon , it will completes the scan of that 100 square degree degrees search area in 0.55 seconds
Not necessary true, Irbis-e is an electronic scanned array, which mean it has various weighting mechanism to reduce the power of the side lobes significantly, whereas APG-66 is a mechanical slotted array radar with predictable scan pattern and much higher sidelobe/main lobe ratio. It should be easier for RWR system to detect and classify a mechanical scan slotted arraysprstdlyscottsmn wrote: RWR might give that info, but I assure you the Su-35s RWR is going to have a harder time picking up the 2-3kW APG-66 compared to the F-16s RWR trying to pick up the 20kW Irbis-E.