If you mean the Super Maneuverability and Thrust vectoring feature, they helps when a BVR engagement do not occur/fails and close combat happens, it is termed as dog fight. Super maneuverability is attained through improved aerodynamic design such as the reverse sweep like wing design and vectoring the engine thrust in a desired/ diverted direction with the help of flexi nozzle type engine exhaust end, which is termed as Thrust Vector.What does the 4th feature mean? Does that give us any clue about engine?
By that time 6th gen fighters will be there in the scenario !AERO INDIA: Advanced medium combat aircraft first flight likely in 2020
New Delhi has adopted a go-slow approach for its planned Advanced Medium Combat Aircraft (AMCA), which is in the early stages of being designed by India's Aeronautical Development Agency (ADA).
"We plan on finalising the configuration by 2018, with a first flight in 2020," says an ADA representative. "The AMCA will draw from what we learn with the [Hindustan Aeronautics-built] Tejas MkI and Tejas MkII."...
AERO INDIA: Advanced medium combat aircraft first flight likely in 2020
But atleast the timeline isn't unrealistic anymore. Also, it mentions that the aircraft will be 20t. Does anyone know if they are talking about empty weight or MTOW?By that time 6th gen fighters will be there in the scenario !
Empty Weight ?But atleast the timeline isn't unrealistic anymore. Also, it mentions that the aircraft will be 20t. Does anyone know if they are talking about empty weight or MTOW?
There are talks of MCA and then AMCA from 2006, today is 2013, Indian govt is really slow in its approach, at least the final configuration should have been finalised till now but this further delay.But atleast the timeline isn't unrealistic anymore. Also, it mentions that the aircraft will be 20t. Does anyone know if they are talking about empty weight or MTOW?
MTOW of course.But atleast the timeline isn't unrealistic anymore. Also, it mentions that the aircraft will be 20t. Does anyone know if they are talking about empty weight or MTOW?
Why is our testing period so long? PAK FA will enter service only in 6 years after the first flight. We would have gained experience on Tejas already.First flight in 2020 would mean an IOC in 2029 and FOC in 2031. That's around the time USN will have their first 6th gen aircraft with USAF to follow up with a 6th gen F-22 replacement undergoing testing.
Well, I suppose that's plenty for us. We will have to start working on a PAKFA replacement by then too. So, another HAL-Sukhoi partnership for a heavy UCAV. Or we may go for it on our own.
MTOW of course.
As a matter of fact, MTOW is expected to be equivalent to that of the F-16 B60.
So, we can expect a 9 tonnes empty weight, 5 tonnes fuel load, 2 tonnes internal weapons and 2x90KN engines. Add another 5 tonnes of external weapons load to the mix. That's plenty in terms of T/W at loaded weight and will be better than all our other aircraft except for the PMF(FGFA) when it comes to performance.
Lack of experience. Twinblade explained that in the LCA thread. HAL was talking about the same. Had they gone alone on PMF, they would still be testing the aircraft 15 years after first flight.Why is our testing period so long? PAK FA will enter service only in 6 years after the first flight. We would have gained experience on Tejas already.
Yeah they are already contemplating to fit 6th gen elements into itBy that time 6th gen fighters will be there in the scenario !
http://www.thehindu.com/todays-paper/tp-national/tp-andhrapradesh/article2664570.eceSince it was planned to have the first flight in seven years, certain concepts of the 6 {+t} {+h} generation combat aircraft would also be incorporated. It was likely to be 10 years for it to get into production for replacing MIG-29 and Mirage fighters.
P2P they dont have experience, but still with all those LCA flying they can easily get carried away and increase the testing to such an extent that they are going to make mistake and lose LCA resulting in closer of programme.Lack of experience. Twinblade explained that in the LCA thread. HAL was talking about the same. Had they gone alone on PMF, they would still be testing the aircraft 15 years after first flight.
With the level of experience and technical know how the Russians will transfer to us we can test the PMF in 4-5 years. PMF needs 5000 hours of flight testing. ADA has taken 10 years to reach 1000 hours on LCA out of 2000 required. Huge difference there.
According to ADA, design stage to first flight is 7 years followed by test flights for 9 years before the induction process starts. That's another 3-4 years. 20 years from scratch to full operational clearance.
With better experience, perhaps we will be able to achieve Russian targets for flight tests.
Can't they shorten that extra 9 years period ? can't we use LCA's testing experience in AMCA ?...
According to ADA, design stage to first flight is 7 years followed by test flights for 9 years before the induction process starts. That's another 3-4 years. 20 years from scratch to full operational clearance.
With better experience, perhaps we will be able to achieve Russian targets for flight tests.
Any LCA crash will not affect the overall program. Especially this far into the program.P2P they dont have experience, but still with all those LCA flying they can easily get carried away and increase the testing to such an extent that they are going to make mistake and lose LCA resulting in closer of programme.
Other have spend time money and gain experience, we are just new kid in the block, before running we need to take baby steps first. We are getting their make no mistake.
There will be massive differences in testing a twin engine aircraft compared to single engine aircraft.Can't they shorten that extra 9 years period ? can't we use LCA's testing experience in AMCA ?
Something I wanted to hearLCA's experience will not see direct replication of similar techniques but the scientists will know what may be wrong and what may be right right from the design stage instead of getting it right on a trial and error basis.