p2prada
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I have already explained that part in the previous post to gogbot. It does not have Gripen like sensor fusion though.you are repeating the same. when the net centicity is achieved and the aircrafts have ODL, they will communicate. it does not matter whether you are on the ground or air.
F22 does not have datalinks?? hillarious. F 22 does not have 'conventional datalinks' but have stealth qualified IFDL which is incompatible with others. it can only communiacte with other F22s.
All development flight tests. The 70deg nose up = AoA. There is nothing else you can imply from it. If the nose pitches up from horizontal to its max possible angle without completely being unrecoverable is the sustained AoA.AOA is one of the parameter not the only parameter to decide aerodynamics. besides LCA is still to secure FOC and here you are comparing it to practically every aircraft under the sun. AOA is a risky business and a new fighter opens to that slowly. check the link you gave for the EF. it talks of 20d and 25d AOA on 2 occasions.
Again. I am only taking "sustained" AoAs. You are talking about continuous AoA'swho is confused?? on the one hand you say 'You are confusing sustained STR with sustained AoA' and on the other 'The aircraft did not stall' - implying AOA!!! shows your understanding.
Do you have STR values of LCA. I doubt it. So, all we have are AoA to go about it.FYI, STR and AOA are intrinsically entwined!! go thro' this and check how it is important to keep 'corner velocity' in a sustained turn and how AOA affects that and hence STR.
http://www.simhq.com/_air/PDF/air_097print.pdf
Also the article is only comparing old aircraft. The Euro Canards are at a different plane of thought when it comes to AoA and other criterias.
does the J 10 video look natural to you?? doesn't it look speeded up?? seems to me atleast. consider this - climb rate is a function of t/w ratio. while J10 has 0.84 at loaded weight F22 has 1.08 at loaded weight and 50% fuel. even with no load on both F22 wins hands down.
I did not post that to show off climb rates. Only AoA.so tell me how a J10 can have a better climb rate than an F22?? don't look at an individual video in clean config (may be tampered) and start passing your judgement.
This was a sustained AoA. The bleeding of energy is a completely different point.SU 30MKI is an exceptionally maneurable aircraft. again this is a momentary exercise and not something which is sustained like in an STR. in an airbattle, i doubt if they have that time. besides that is not my point anyway.
You are detracting from the point I made in the first place. LCA Mk1 cannot even do half of what other aircraft can do.whether you call it continuos AOA or i call it sustained AOA 'does not change' the point i am making.
Aircraft like F-16 don't need High Alpha AoA in a dog fight. But aircraft like LCA which relies on climbing and diving need high AoA with high TWR.
F-16 relies on STR.in air combat pilots will use every tactic they can employ to get the better of the opponent. if it means employing momentary high AOA there is nothing to object to because the factors like bleed, drag are not an issue while in a sustained AOA all of them are part of the picture - while one's aim is to sustain the fight by conserving energy and remain engaged and defeat the enemy!!
F-15, Mig-29 Su-30, LCA Mk1, Mirage-2000, EF-2000, Rafale and other non TVC aircraft rely on diving and climbing manuevers.
Gripen relies on STR as well as diving and climbing. They have both advantages simply because it's a 21st century plane. The LCA, even after being a later design than Gripen cannot even do half the things Gripen does.
All low speed maneuvers.now does that affect the maneurability of the Mirages?? take a look at this video -
Check this video and compare with what you posted. All high speed maneuvers with better performance.don't sell your prejudiced POV here.
Somehow I am the prejudiced one.
That's why Mirage-2000 and LCA Mk1 are dead designs. Without LERX or Canards, they are just obsolete designs.F16 is cropped delta while Mirage 2000 is compound delta. just look at the wings. Mirage will burn and bleed more energy in an STR. that explains the whole thing. Mirage or an LCA will not go into STR with F16 for the reason i have explained before.
LCA Mk2 model is being shown in Aero India 2011. You will hear it first here before any journo gets his hands on the first pic,
The LCA Mk2 Will have LERX.
There you go with specs again. The Mirage-2000 was and LCA Mk1 could have been frontline aircraft in the 80s and 90s. But not any more. They are dead designs. Just watch the Gripen video and compare.let's do some math at common loaded weight for Mirage 2000 and LCA mark 1.
Mirage 2000---7500+3978+100+910=12488 and @ 95.1kn gives a T/W ratio of 0.78
LCA mark 1----6500+2486+100+910=9996 and at 85kn gives a T/W ratio of 0.87
there goes your 'underpower' hypothesis.
if Mirage can stay as frontline aircraft at much less thrust how can't LCA mark 1 at higher thrust??
Haha! You are comparing superior airframe design on Gripen with inferior airframe design on LCA. Both have the same engines.besides i gave the same math wrt Gripen C where again LCA mark 1 scores!!! if thai/czekh/south african AFs think like you they would have never inducted Gripen. there are whole lot of considerations other than T/W.
If the Thai, Czech or South Africans were comparing Gripen and LCA(fully ready with similar avionics). They would definitely go for Gripen even if LCA gives higher thrust.
Will repeat, LCA Mk1 is a dead design. It no longer holds any place in modern air warfare. Only 40 aircraft and a grim but sarcastic ACM are proof of that. They will see early retirement and a decent burial.
It's the ACM who is glum, it's the ACM who is sarcastic on national TV and it is the ACM who says the LCA has a loooong way to go and somehow I am the prejudiced one. However I would rather be called Prejudiced than Gullible.
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