Firstly JF17 Block 3 comes with RD93MA engine not RD93.
Second PFX is not the need of today but at least 10-15 years from today.
Russian Al-51F1 and Chinese WS15 may provide enough thrust and power for our pfx requirements.
We are not making a high-end fighter like F22 or J20!
It will be a lighter fighter as compared to them and some compromise on some features maybe made.
We are not thinking of trying to compete chinese in this Industry but will benefit from chinese expertise or may get some turkish help.
PFX will be a "low" in PAF's "high-low mix" strategy.
Regards.
Please go back to your original vision! This is the center of our dispute!
PFX will purely be a fifth gen fighter jet.
On the other hand PFX will be a single engine 5th gen jet to form the future backbone of Pakistan Air Force.
If it is equipped with a single high-thrust turbofan engine (AL-51/WS-15), it will be upgraded to a medium-sized fighter. This overlaps with the J-35's positioning. A country does not need to use two 5th-Gen fighters at the same time.
I'll give you some data to help you understand.
1. The performance improvement of the RD-93MA over the RD-93 is small (about 10%), with the main improvement being in launch life rather than performance. Its maximum generating power: 30~45KW. when its generating power exceeds 30KW, the propulsion provided to the fighter by the engine starts to show a decline. When its generating power approaches 45KW, the fighter cannot perform mission maneuvers that consume energy.
The 4.5th-Gen fighters, depending on different configurations (different levels of sophistication), the maximum power consumption is usually around 40~70KW.
The minimum standard for 5th-Gen fighters is 150+KW. The current 5th-Gen fighters (F-22/F35/J-20/J-35/Su-57) all have engines that provide a maximum power generation of 150~200KW. the KF-21/KAAN/AMCA, They have engines now that are not up to that standard. They actually belong to the 4.5th-Gen fighters now.
2. There are a lot of avionics equipment on the fighter jet. Flight control system, mission computer, radar, EWS, warning system, navigation system, cockpit system, communication and data link ......
I only analyze the radar system of JF-17B3. Please understand other systems on your own.
The KLJ-7A radar was originally available in three versions. A base version (liquid-cooled heat sink) and two higher-order versions (mechanically deflected array antenna/side-view antenna array).
However, PAF ended up customizing a special version of the base version for the JF-17B3. The antenna area was reduced (lowering the number of T/R modules), and the cooling was changed from liquid-cooled to air-cooled (lowering the energy consumption of the cooling system). It fits the nose size of the JF-17, and at the same time it consumes much less power, making it easy to accomplish the modification. Of course, the cost was also lower. However, the performance is also drastically reduced.
KLJ-7A radar. The maximum power of one T/R module is 10~15W (limited by heat dissipation capacity). If calculated based on 1000 T/R modules, the maximum power will be 10~15KW. This does not include the power consumption power of the other parts of the whole radar (thermal management system, back-end processing system, auxiliary sensors and calibration system, etc.).
According to some in-depth research data, the thermal management system of the KLJ-7A air-cooled version of the JF-17B3 radar can only support a maximum of 8KW.
Yes, it is a radar whose performance is “severely curtailed” because of “the lack of blood supply to its heart”. But PAF made that choice!