Sources, please.
The U.S. Naval Institute
The Naval Institute guide to world ... - Google Books
Plus, here's another source.......
Of the current generation of US AESA radars, the only one which is well technically documented in the open literature is the APG-79, which will therefore be used as a baseline for comparison against the Flanker radars. Of the current generation of U.S. AESA Radars, the only one which is technically well documented in the open literature is the APG-79, which will therefore be used as a baseline for comparison against the Flanker Radars.
The APG-79 was initially sold as a block upgrade to the legacy APG-73, itself an incremental upgrade to the APG-65. The APG-79 was initially sold as a block upgrade to the APG-73 legacy, itself an incremental upgrade to the APG-65. The APG-79 however ended up being much more than a simple block upgrade, adding not only a powerful AESA, but including additional processing capability and tight integration with the ALR-67 radar warning and emitter locating system, and requiring forward fuselage changes to the aircraft. One of the key design considerations was to improve the capability to detect and engage anti-shipping cruise missiles, a major problem for the US Navy Carrier Battle Groups. Given the relatively modest footprint to be defended, the poor supersonic performance and payload range of the Super Hornet was less important than the ability to lift an X-band radar above the horizon of the shipboard defences. The APG-79 however ended up being much more than a simple block upgrade, adding not only a powerful AESA, but including additional processing capability and tight integration with the ALR-67 radar warning and emitter locating system, and requiring changes to the forward fuselage aircraft. One of the key design considerations was to improve the capability to detect and engage anti-shipping cruise missile, the major problem for the U.S. Navy Carrier Battle Groups. Given the relatively modest footprint to be defended, the poor performance supersonic range and payload of the Super Hornet was less important than the ability to lift an X-band radar above the horizon of the shipboard defense.
There is enough unclassified data available at this time to perform a reasonable estimation of performance bounds on this radar, with the caveat that evolving transistor technology over the life cycle of the design will see shifts in performance. The radar is known to have ~1100 modules , which assuming like per module power rating, cooling and X-band wavelength would result in around 70 percent of the power rating of the APG-77 . This puts the radar broadly between 10 kW and 20 kW peak power ratings . There is enough unclassified data available at this time to perform a reasonable estimation of performance bounds on this radar, with the caveat that evolving transistor technology over the life cycle of the design will see shifts in performance. The radar is known to have ~ 1100 modules , which like assuming per module power rating, cooling and X-band wavelength would result in around 70 percent of the power rating of the APG-77. This puts the radar broadly between 10 kW and 20 kW peak power ratings. Public data comparing the APG-71, APG-73 and APG-79 yields an indication that the radar has similar power aperture product performance to the 10 kW rated APG-71, which for half the antenna area yields a peak power rating of the order of 20 kW. Public date comparing the APG-71, APG-73 and APG-79 yields an indication that the radar power aperture product has similar performance to the 10 kW rated APG-71, which is half the antenna area yields a peak power rating of the order of 20 kW. This data supports the proposition that the radar is a 20 kW peak power class design . This data supports the proposition that the radar is a 20 kW peak power class design.
In general, the peak power rating of an AESA is determined by the per module power rating multiplied by the number of elements, with some reduction resulting from the taper function which is used to weight power output per module, so that sidelobes and mainlobe shape can be optimised.
A 20 kW peak power AESA with a 15% allowance for taper function yields for instance a per module rating, for 1100 modules, of around 21 Watts. The average power output of the radar is then limited by the duty cycle of operation, and power consumption overheads incurred by drivers, and phase and control elements in the modules. In general, the peak power rating of an AESA is determined by the per module power rating multiplied by the number of elements, with some reduction resulting from the taper function which is used to weight output power per module, so that sidelobes and mainlobe shape can be optimized. The EFSA 20 kW peak power with a 15% allowance for taper function yields for instance the rating per module, modules for 1100, of around 21 Watts. The average power output of the radar is then limited by the duty cycle of operation , and power consumption overheads incurred by drivers, and phase and control elements in the modules.
The latest engineering literature on AESAs puts the state of the art for radiated X-band power intensity at about 4 Watts/cm2 which for the X-band is around 16 Watts/module. This would put the total peak power at about 17.6 kW . The latest engineering literature on AESAs puts the state of the art for X-band radiated power intensity at about 4 Watts/cm2 which is the X-band is around 16 Watts / module. This would put the total peak power at about 17.6 kW.
Many sources available..........
Sorry, I am done playing........
Raytheon APG-79 AESA (U.S. Navy image).