black eagle
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The headphone crackles in his ears as Wing Commander Pranjal Singh looks out from the cockpit of his Tejas Light Combat Aircraft, codenamed LSP-3, at the sun-baked runway stretching ahead. Once again he blesses the Indian designers who built the Tejas cockpit: in the Sukhoi-30MKI that he flew before test pilot school, he would have been dripping sweat.
Group Captain George Thomas, built like a bull, has commanded a squadron of Su-30MKIs. Group Captain Ritu Raj Tyagi, the most experienced of the group and a former Jaguar combat commander, ran the last Mumbai marathon as a diversion from flight testing. Captain Jaideep Maolankar, who cut his teeth flying Sea Harrier fighters off naval aircraft carriers, commanded warship INS Ganga as it chased pirates off the Somali coast. Group Captain Venugopal, like Varma, has commanded a MiG-21 squadron on the Pakistani border.
Even Pranjal, the baby of the team, is by conventional standards a veteran pilot, having commanded a Sukhoi-30MKI squadron. Now learning the ropes at the NTFC, he will extensively test the first two Tejas fighters that Hindustan Aeronautics Limited delivers to the IAF this year.
The LSP-3 streaks into the sky. Pranjal's mission is to test a new smoke winder--an under-wing pod that trails smoke. The device will help the NFTC test the Tejas' reaction when it flies into a jet wake, a deadly 250-kmph blast of air emitted by a jet engine flying ahead.
Jet streams confuse fly-by-wire fighters like the Tejas, which are kept stable by on-board computers. Swedish company Saab crashed one of their Gripen fighters during testing when it flew into one. But these NFTC pilots seem to believe that flying the Tejas into a jet stream is just another day at the office. This matter-of-fact approach to the unknown leads NASA to choose most of its astronauts from the test pilot community.
In western air forces, like the US Air Force, test pilots do nothing but flight testing. But while specialisation allows them to stay in close touch with test programmes, pilots become disconnected from combat flying. The IAF's philosophy is different. "Our tactics are evolving so quickly that we feel it is better to keep moving pilots between test flying and operational squadrons. That brings the latest operational doctrines into aircraft development," explains Thomas.
Thanks for the information Rage!! Any idea about avionics package decided for MkII.. Will AESA radar be ready by that time?? I heard sometime back that pylons are to be made little wider for two extra hard points!!..
We don't need a canard:simply, because this is a compound wing. The rearward-sweep angle of a compound wing vastly lowers the airspeed normal to the leading edge of the wing, generating useful lift, essentially performing the function of a (lifting-)canard, with very low wing-per-unit loading. On the other hand, a control-canard, such as on the Mirage-III S, has very poor stealth characteristics. A canard-delta would also suffer from smaller shifts in the center of lift with increasing velocity, particularly at already high speeds. One conceivable benefit of control-canards could be the reduction/avoidance of pitch up, but those are mostly for swept-wings, and I haven't seen the LCA encounter that problem. Besides, redesigning an airframe and wing structure to accept canards is not without problems, including changes in fuel-centre of gravity, induced drag incompatibility /changes in max lift coefficients, directional stability and the lack of winglets/ wing fences, distortions in additional load distribution on the wings, etc. A close-coupled canard might be considered, but I think that could lead to too many additional complications.Adding:
Why can't ADA think of having a 'Canard' to improve the lift!. As the fuselage is extended a bit will it be effective to have a control-canard in MkII?? Will that add better maneuverability for the bird??
Perhaps weight might be the issue there.See i don't get why the LCA mkII can't be the same as the LCA-N and use LEVCONS
Gripen has wing tip pylons mate. Wing tip pylons = cropped. And the rest as you said.@P2P
Gripen is more like a pure delta enhanced with canards. it has a modified trailing edge for better control surface actions. JF 17 is a delta with LERX....
Well in ACM with a delta...not even a rookie pilot will do a 180 degree...he rather go in for a Immelman's turn...he will lose lesser energy doing it....one needs to fight with the strengths he has knowing the weakness and strengths of the enemy. LCA will fight in the vertical after the merge..it would be stupidity to turn with the opponent. The Compound delta has it's own advantages like maintainance issues and climb performance with lesser drag (that's what was actually envisaged). I would not call a compound delta completely useless..remember the actual GSQR was for the replace meant of the Gnat and later on shifted to MiG 21.Compound is next to useless in medium and low altitudes. Sure, LCA is useful over Himalayas, but Cropped would have been even better. Saab introduced Canards on their compound delta Viggen and it gave it pretty good performance at low speeds. But LCA, I am not so sure. It's just gonna fly fast and straight before making a Massive 180 deg turn before trying to get into the enemy's backside.
I was joking when I said 180 deg turn mate. Notice the word Massive with capital 'M.'Well in ACM with a delta...not even a rookie pilot will do a 180 degree...he rather go in for a Immelman's turn...he will lose lesser energy doing it....one needs to fight with the strengths he has knowing the weakness and strengths of the enemy. LCA will fight in the vertical after the merge..it would be stupidity to turn with the opponent. The Compound delta has it's own advantages like maintainance issues and climb performance with lesser drag (that's what was actually envisaged). I would not call a compound delta completely useless..remember the actual GSQR was for the replace meant of the Gnat and later on shifted to MiG 21.
Hey the AoA itself is a classified info that we are flouting around in the open...I think LCA has the highest number of articles criticizing it's AoA. yes keeping up with sustained AoA is difficult...but LCA was never meant to be 1 vs 1. It is an interceptor and they hunt in packs.I was joking when I said 180 deg turn mate. Notice the word Massive with capital 'M.'
Lag Roll and High G Barrel Roll come to mind with the LCA, with the defensive spiral to evade. I am guessing LCA is more of a team effort fighter than a 1vs1. Wingman etc will be involved after all. But all aircraft with High AoA like MKI or Gripen will evade these maneuvers easily. The last I heard even F-16 had a hard time against High AoA maneuvers compared to high G maneuvers in 2006. For eg: I doubt the LCA can perform the Tail slide as easily as the Gripen does, if it can do it in the first place.
Anyway, any idea what is the roll rate of the LCA?
ADA announced the AoA figures, it's not speculation. AoA isn't secret because people can see it. Also I am not hung up on AoA. With just compound wings without vortex controllers the AoA will not exceed 35 deg or risk a deep stall. It's a risk that will be carried out in test flights though. So, final AoA figure is up to speculation. Information will be released upon achieving it. The N-LCA with LERX may handle more considering they need it for carrier landing and take off.Hey the AoA itself is a classified info that we are flouting around in the open...I think LCA has the highest number of articles criticizing it's AoA. yes keeping up with sustained AoA is difficult...but LCA was never meant to be 1 vs 1. It is an interceptor and they hunt in packs.
Yes I agree with you. But LCA has it's flaws just like other aircraft...MK2 is what is the actually envisaged ASR...not the MK1...but I think the LCA MK1 is a far better choice as a stop gap measure instead of upgrading the MiG 21s.ADA announced the AoA figures, it's not speculation. AoA isn't secret because people can see it. Also I am not hung up on AoA. With just compound wings without vortex controllers the AoA will not exceed 35 deg or risk a deep stall. It's a risk that will be carried out in test flights though. So, final AoA figure is up to speculation. Information will be released upon achieving it. The N-LCA with LERX may handle more considering they need it for carrier landing and take off.
Normally cropped deltas handle very high AoAs with vortex controllers and we already see that on Rafale(32 deg FCS and XX deg beyond that), MKI(80deg with FCS+TVC and xx deg beyond) etc. Perhaps with the design optimization on LCA Mk2 we may end up with a Mirage-2000+ by 2016 or even a Mig-21++.
We have no idea what else they are planning on the Mk2. Compound deltas cannot handle too much engine power especially considering LCA's wing loading is already very low. So, touching 114 or 115KN will be too much on the F-414 for the LCA. If IAF is not expecting Mk2 to go beyond what is specified then the engine power will be cut back to 100KN as they originally wanted. Unless of course we are getting the EPE version or something.
Satish, the enemy fighters will be in packs too.
thanks Nitesh for that LCA video. most spirited and beautiful display ever seen by me.nice video:
also check the experience put in for the testing:
http://ajaishukla.blogspot.com/2011/02/men-and-their-flying-machine-day-at.html
But not the one we built. It's currently at Mach 1.6 and only at high altitudes. The last I heard, it goes transonic at low altitudes. And G limits are -3.5/8.The compound delta can handle high speeds.
I like the F-22 formation. The middle finger thrust......*jokes jokes*All fighters move in packs...the most preffered interception formation is the finger four.
It is indeed a fantastic display, thanks to the person who shot it (Dr, shiv), quite energetic display, also by seeing the gamut of experienced pilots testing this baby is a positive sign.thanks Nitesh for that LCA video. most spirited and beautiful display ever seen by me.
half a barrel roll...flying inverse...reverse vertical loops...tight banking turns...full barrel rolls...steep climbs...
wow. and it will only get better from here!!! who needs canards for this?? ADA was afterall correct in their design. well done.
also thanks for the nice article by Ajai shukla.
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