You can say so if you want, because LCA is in a development, where it is limited to something between 6 and 8Gs. But at the same time LCA has better dry TWR and lower wingloading and the same speed, so can you say JF 17 block 1 standard is generally more maneuverable then the LCA MK1 standard?
He can't because he only speculated about the possible capability, with the arguments that China has developed a stealth fighter and that PAF has said it is near F16 Block 50 standard. The earlier is a fanboy claim, the later is not reliable but tells you something, that the avionics are propper 4th gen standard, but possibly below US export avionics.
Btw:
http://www.defence.pk/forums/pakist...lca-development-comparison-9.html#post3625033
Claiming Israeli techs are allways the best is not reliable either of course, but compared to the Chinese case, we can find way more publically available specs, infos, reports about them. We know that the Dash HMS is one of the most mature and best helmets available, we know nearly all specs of the Litening pod and that even US forces prefer to buy them buy them, so we come to a conclusion about them, which is not the case with most Chinese techs.
No he is not and that's what I tried to make you understand in the last point, the 150Km are the detection for fighter class targets of 5m2 the common used target size of radars in this generations, the detection for bigger targets like transport aircrafts, tankers or ships for example is far bigger be it for EL 2032, KJ 7, KJ10, or Zhuk ME, but manufacturers commonly point out the detection against fighter sized targets.
You can easily find publically available specs for numerous radars:
EL 2032 - 80nm ~ 148Km (
http://www.iai.co.il/sip_storage/FILES/0/38030.pdf)
Zhuk ME - 120Km (
http://img455.imageshack.us/img455/2257/zhukmeav9.jpg)
KJ 7 - 105Km (
http://1.bp.blogspot.com/_44d3OT-xI...Azw/6KlQvpDYNfY/s1600/JF-17+Thunder's+MMR.JPG)
More modern radars like RBE 2 PESA, or Captor M of Rafale, EF, or Russian Flanker, or modern AESA radars are always rated against targets of 3m2. That's why I said, he even get that wrong, because no manufacturer rates his maximum A2A detection against the biggest possible target.
Based on? My points are made in the comparison above.
Of course and still you do more than 2/3rd of the mission with dry thrust, be it even just to safe fuel in CAP, so AB thrust is not the important one. That's why the Swedes for example focused of dry thrust of the RM 12 engine, while the AB thrust is lower compared to GE 404, although it is based on the GE 404. Or why Supercruise capability is an advantage, because it makes you fly at high speeds without the use of AB.
True, neither does the unit cost and still he said that's a reason why JF 17 is superior isn't it? But either you look at both sides unbiased and equally, or you shouldn't bother to do such comparisons and the autor of your comparison had obviously a very one sided view!
- no i dont say that block I standard is more maneuverable than LCA MK-1...but as of now yes jf 17 is MORE MANEUVERABLE...thats for sure..
dry TWR and lower wingloading:-
does A BIT HIGHER TWR (supposition) helps LCA to be better in WVR with a ristricted AoA and the G-LIMIT ?
ahh..please i think we should not go into details of TWR..it fluctuates according to mission circumstances,
but assuming both of these jets under same circumstances and same mission status...i.e same weapon payload
first off,this is highly unlikey the case,we are discussing on paper...
secondly even if both are carrying same payload and flying with dry TWR...i should remind you that LCA is heavier than jf 17 i.e more empty weight...
so AT THE SAME TIME jf 17 has still advantage...( as of now )
coming to lower wing loading..it has its advantages and disadvantages as well...low wing loading gives superior sustained turn rates,superior climb rate,better high altitude performance and better service ceiling...
while jets having higher wing loading like jf 17 is in the case...have some advantages too,
like more suited for high speed flights,superior instantaneous rates,BETTER low altitude performance..
so the LCA should have following advantages:
superior sustained turn rates but its negated by the G-tolerance limit..i.e 6 as of now
superior ceiling and climb rate...but jf 17 has got better ceiling..
jf 17 holds an edge in instantaneous turn rates,service ceiling,better AoA and G-LIMIT...
SO WHICH IS MORE MANUVERABLE ...its offcourse the jf 17...( not talking about FOC standards )
- yes he cant and neither did he not say clearly that jf 17's avionics package was BETTER...hence he is NOT wrong on what he said...
similarly indians too, can not say that LCA has better avionics package...
- RADAR RANGES :-
he seemed to be taking the ranges in air to air mode...where he is more or less correct...
tejas has UPTO 80 NMI for air to air... ( no source available quoting range for 5m2 )
jf 17 has 105 km for 5m2...( no source is available quoting max. air to air range of KLJ-07 )
so assuming both radars have detection and tracking ranges lieing in close vicinity is not wrong...
yes its mere an assumption but you cant prove it wrong either..
- RCS:-
how can you claim that RCS of tejas is lower?
do we know RCS of tejas...NO
do we know RCS of JFT..NO
as far as my brain helps me...
small size, less reflecting surfaces, use of RAM coatings and high use of composites materials can reduce the RCS...but can not bring lower than 1...
same is the case with jf 17..like we heard many of think tanks including pshamim saying jf 17 has lowest RCS among all the jets including block 52 in PAF's fleet...as of now...
DSI,limited use of RAM,small size may also be sufficient enough to bring RCS around 1...
- yes unit cost too,does not affect performance in air
BUT,engine operational cost is not that big issue...and PAF is happy with engine performance..
on the other hand the high over-running cost of LCA actually shows that how successful the project has been...