Haavarla
Active Member
The Tikhomirov NIIP L-band AESA has considerable growth potential by virtue of the large size of the Flanker airframe, permitting additional antenna elements, cooling and power.
Growth options include:
Increasing the power rating of the existing TR modules, retaining conduction cooling.
Further increasing the power rating of the TR modules and introducing liquid cooling.
Improvements to antenna element design to increase element gain.
Extending the arrays further along the wings, to add an additional one or two subarrays.
Addition of receiver arrays in the leading edge of the vertical tails to provide dual plane monopulse precision angle tracking capability for fire control purposes.
For instance, increasing the array size to 16 elements improves power-aperture product for the existing design by almost 80%, by virtue of additional gain and transmit power. The use of more powerful TR modules provides for further improvements. The practical limit will be the available leading edge flap volume as the design progressively tapers toward the wingtips, and system constrains on liquid cooling capacity.
http://www.ausairpower.net/APA-2009-06.html
Ok, lets hear any toughts about this systems. Its growt potencial, etc etc?
Thanks
Growth options include:
Increasing the power rating of the existing TR modules, retaining conduction cooling.
Further increasing the power rating of the TR modules and introducing liquid cooling.
Improvements to antenna element design to increase element gain.
Extending the arrays further along the wings, to add an additional one or two subarrays.
Addition of receiver arrays in the leading edge of the vertical tails to provide dual plane monopulse precision angle tracking capability for fire control purposes.
For instance, increasing the array size to 16 elements improves power-aperture product for the existing design by almost 80%, by virtue of additional gain and transmit power. The use of more powerful TR modules provides for further improvements. The practical limit will be the available leading edge flap volume as the design progressively tapers toward the wingtips, and system constrains on liquid cooling capacity.
http://www.ausairpower.net/APA-2009-06.html
Ok, lets hear any toughts about this systems. Its growt potencial, etc etc?
Thanks