Kowsar could be made as effective as F-14 by making these choices:
- no automatic cannons on the aircraft.
- new nose for the aircraft to house larger radar.
- new air to air missile that at most is 500lbs in weight.
- with modern manufacturing should allow new AAM an AIM-54 range.
- landing gear on wing removed, lighter wing with fuel storage capacity.
- new landing gear at rear similar to Su-25 or MiG-23 at very least.
- RD-33 equivalent low bypass turbofan without afterburner.
- thus weight comparable to two J85 and length too to J85.
- longer range, endurance and top speed of Mach 2 clean.
- most notable would such able to do super cruise.
The above tallies what I have surmised also, barring a few differences.
- No auto cannon (the Vietnam war has shown this to be an error in judgement - there is a photo-shopped image of Kowsar showing a single barrel cannon dropped to the lower cheek, port side).
New nose for larger radar. Check. See
https://defence.pk/pdf/threads/jf-17-thunder-still-under-evaluation-by-the-plaaf.150839/ for instance, and consider also Iran's own Shafaq.
- New AAM weighing at most 500lbs. (Check ... AIM-120D weighs 358 lbs. R-77M, weights 419+ lbs. This is from the R-77-1. PL-15 - comes in at 419 lbs. And finally the Meteor, also 419lbs). All of these missiles have a range of 150 - 200+km.
- modern manufacturing should allow a new AAM an AIM-54 range. Doable. Besides modern manufacturing - think newer, lighter, material - hybrid solid fuel, and also an improved guidance system resulting in a more energy-efficient trajectory. All the aforementioned pushed Sayyad-4B's range up from 200km(4A) to 300km.
- landing gear on wing removed, lighter wing with fuel storage capacity: Check, check, check. Wings like Iran's cranked delta, and add. fuel with permanent CFT's. While I agree with the removal of the landing gear.
- new landing gear at rear similar to Su-25 or MiG-23... I will err on the side of caution and simply say that I do not have the foggiest of how much tinkering and panel beating this would require. Nevertheless, I will still adjudge this as a check. Just wonder if the automatic gear reportedly first fielded on Saeqeh some years back could tribute something to this end?
- Regarding a RD-33 equivalent low bypass turbofan without afterburner. I do not agree as there are a/c such as the F-20 Tigershark L =14.43 m; JF-17 Blk-3 L =14.33m; JAS-39C Gripen L=14.9m; and the Tejas Mk 2 = 14.65m. All those aircraft have engines roughly in the size and thrust class of the RD-33, All with A/B. The a/c on which this new iteration of Kowsar will likely be base is the Saeqeh II. The 2 seater has a L =~15.89m, depending on the source consulted. So the propulsion, say RD-33 with AB, should not present intractable problems being fitted to a single seat Kowsar.
- longer range, endurance and top speed of Mach 2 clean. By way of example, the F-20. It has a CAP of 138 minutes on station + 20 minutes reserve at 560km. For hi-lo-hi interdiction its 1,020 km. F-20 has a top speed of M=2 so I assume Kowsar will follow suit. Another tick.
- most notable would such able to do super cruise. I have not come across such info regarding F-20, and by implication also a 'new' Kowsar. Will have to wait until a new Kowsar become public and data starts to emerge.