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We can hv a meaningful, informative , discussion With mutual respect, on tejas, with 0 input from trolls & shills. No need to engage Trojans. These guys are totally exposed here now. They are free to sing their own tunes, with their own company of mutual admiration society.

Nice post!!! You hv used the word sh!t only once, Good improvement. I dont really care for you judgements on me, It is really satisfying to know, that the forum has an ,"expert" who knows more than the Mods!!! You can from now on guide the thread & mods with your golden rules of ,"FIGHTER...

Problem is the toxicity you bring in with your foul mouthed convo skills Long arguments & heated discussions are not new to this thread. I am posting here for close to a decade. Don't lie & mislead people. This thread was once cited in CAG report.There is a thread on that too, Mods hv...

Other than toilets , septic tank, defa,,,,tion analysis, like the above, What's your contrtibution to this thread? Oh, .I forgot,,, Crying for help to your friends!!!! ROFL.

After lying thr After lying through out this thread on Wing loading, engine thrust can do the job of balancing CG, CL, margin of instability, with no need for weight balancing, Trans sonic wave drag operates in subsonic speeds, it is cumulative, continuum from, not binary etc, etc, &...

You just keep all holes of your body tightly shut up ,when it comes to snidely insulting me, Why would I waste my time replying to you?

http://sturgeonshouse.ipbhost.com/topic/188-a-quick-explanation-of-relaxed-stability/ Has some fantastic explanations, Delightful read

Yo mud headed expert, Read the following, Before starting your ,"fortune telling", "Combined with relatively low wing loading andpowerful basic flight controls, it makes for an exceptionally agile aircraft, controllable even at very low speeds and high angle of attack. " You hv been yelling...

In negative stability (Relaxed Static Stability, RSS) fighter like Tejas, Center of Lift (CP or CL) is in front of Center of Gravity(CG), So that the fighter is UNSTABLE in pitch axis & goes with the wish of pilot trying agile manuoveres, They need precise analog or digital flight control...

1 December - The PV-3 flew for the first time for 27 minutes at an altitude of 2.5 km and at a speed of Mach 0.8. The PV-3 was equipped with a more advanced pilot interface, refined avionics and higher control law capabilities compared with the previous versions. 2007 Tejas PV-1 firing an R-73...

How ironic, After 10 years we are once again starting the same kaveri snecma jv rejected by IAF,, IAF rejects French offer on engine for Tejas Ravi Sharma -------------------------------------------------------------------------------- ‘Kaveri’ under developmentat the GTRE for 20 years...

https://defenceforumindia.com/forum/threads/ada-tejas-lca-news-and-discussions.1/page-422 Firstly, as testified by the IAF test pilots who have flown the Tejas through more than a thousand hours of flight-testing, the current version of the fighter, i.e. the Tejas Mark I, is already a...

Above quote of Air Marshal Matheswaran at Vayu Stratpost conference, Underlines the perils of giving control of deep tech orgs like GTRE, ADA, HAL to IAF personnel , Who hv no technical credentials . These guys, who hol forth on this subjects, about which they hv no clue will destroy...

https://defenceforumindia.com/forum/threads/ada-tejas-lca-news-and-discussions.1/page-422 There is a tejas picture in that page, With a poster infront stating tejas mk1 has 2 hrs 30 minutes maximum endurance

The poster in front of Tejas mk1 in Aeroindia says, It has max endurance of 2 hrs 30 minutes

On page no 421 in this thread, A full report on Air marshal Mateshwaran's speech at vayu round table is available, https://defenceforumindia.com/forum/threads/ada-tejas-lca-news-and-discussions.1/page-421 Excerpt from this, "Cost and time frames are absolutely unrealistic. And example: the...

How does fighter design starts? A hypothetical scenario, ASR specifies, Range, weapon load, close combat specs like ITR, AOA, TWR of entire fighter,Max G,STR, roll rate, climb rate etc, Designers decide, With the available engine tech, & engine TWR, Whether it is possible, Or, Not. Give...

The following BR post about flutter test may esse the confusion regarding that 1350 kmph flight speed at sea level forums.bharat-rakshak.com/viewtopic.php?f=16&t=5058& This is Vina's post, interesting. The document at http://www.aero.iisc.ernet.in/kartik/INCAST_sudha5.pdf at page 5 is very...

This what the Derisively called "MIG 21 class fighter ", is doing to fledgling indian mil aviation sector, Most of the modules and components have been outsourced by HAL to the private sector. Wings are manufactured by L&T at its Coimbatore unit. T Front fuselage-Dynamatic Technologies...

And the words of the IAF Men who matters, interview of Air Commodore (retd.) Rohit Verma. He mentioned that he could again fly a single seat Tejas by just undertaking 2 sorties in the simulator instead of going through a dual check flight, like he would if he flew a MiG-21 again. When he...