abdulbarijan
PDF THINK TANK: ANALYST
- Joined
- May 15, 2010
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I find it really funny, how the thread is started with the whole tirade of " Don't derail this thread" and how this thread is concerning "certain design aspects" concludes in how "IAF IS ON THE RIGHT TRACK"
Two serious points though
- The exact wing area of JF-17 might not even be known, I've seen the 24 odd square meters figure from the time PT01 was around. The production JFT is based on PT-04 with LERX, which in of itself provides more wing area and as a resultant a lower wing loading. Just a comparison ..
-As far as engine power is concerned, here is a summarized version of all the credible information available on the engines and as a resultant the T/W ratio.
Poster for the claims by Kilmov - ( The manufacturer of the RD-93 engine.) stating the thrust from 79-98 KN.
Quote of Wg Cmndr. Ronald Felix regarding the engine thrust ..
Our very own contributor @Tempest II reporting back from Farnborough, UK in 2010 ...
Squadron Leader Nadir Ali around 2 minute mark in the following video...
In addition, you have the vertical takeoff at Paris, with the tires out producing a huge drag yet the jet still goes in to a vertical climb ... There are also snippets of good vertical performance in the Zhuhai airshow 2011, and Paris air show 2015. In addition you can also look at the following video where you see quite aggressive climbing performances ..
The sources that mention the 19,000 lbs class thrust are as following ..
Izmir airshow chart 2011 - 19391 lbs or 86.2 KN
PAFWallpaper.com - 19391 lbs or 86.2 KN
PAC poster at IDEAS - 19200 lbs or 85.4 KN
PAC website - 19,000 lbs or 84.5 KN
Even among these sources we can see quite a variation, the latest claims come from the pilots who fly the aircraft, be it Wing Commander Ronald or Sq Leader Nadir ... the engine thrust is rated as quite high which gives a T/W above 1 .. which has been practically demonstrated in the Paris airshow ...
Two serious points though
- The exact wing area of JF-17 might not even be known, I've seen the 24 odd square meters figure from the time PT01 was around. The production JFT is based on PT-04 with LERX, which in of itself provides more wing area and as a resultant a lower wing loading. Just a comparison ..
-As far as engine power is concerned, here is a summarized version of all the credible information available on the engines and as a resultant the T/W ratio.
Poster for the claims by Kilmov - ( The manufacturer of the RD-93 engine.) stating the thrust from 79-98 KN.
Quote of Wg Cmndr. Ronald Felix regarding the engine thrust ..
Our very own contributor @Tempest II reporting back from Farnborough, UK in 2010 ...
Now, I have slept and rested after a loong day at the show and can write a little bit more:
- Concerning the TWR, he said this after I specifically asked about the thrust of the RD-93. I was asking this because I still find it hard that the RD-93 is based on RD-33 Series 1. The pilot then said to me, "What I can tell you is the thrust-to-weight ratio. Do you know what that is?" I said "yes". And he said, the RD-93 will give the plane a TWR of over 1:.1.1." I started asking about the loading conditions (how much fuel and minutions) it will be carrying to come to this figure. He got his attention take away by other ppl and then they had to go and do a TV interview.
Squadron Leader Nadir Ali around 2 minute mark in the following video...
In addition, you have the vertical takeoff at Paris, with the tires out producing a huge drag yet the jet still goes in to a vertical climb ... There are also snippets of good vertical performance in the Zhuhai airshow 2011, and Paris air show 2015. In addition you can also look at the following video where you see quite aggressive climbing performances ..
The sources that mention the 19,000 lbs class thrust are as following ..
Izmir airshow chart 2011 - 19391 lbs or 86.2 KN
PAFWallpaper.com - 19391 lbs or 86.2 KN
PAC poster at IDEAS - 19200 lbs or 85.4 KN
PAC website - 19,000 lbs or 84.5 KN
Even among these sources we can see quite a variation, the latest claims come from the pilots who fly the aircraft, be it Wing Commander Ronald or Sq Leader Nadir ... the engine thrust is rated as quite high which gives a T/W above 1 .. which has been practically demonstrated in the Paris airshow ...