Guys,
Can you please share your expert comments as why the IAF did not accept the Kaveri Engine?
As I was reading about Aero Engines, I got surprised to learn that Kaveri in fact had more thrust (both dry and after-burning!) than even Snecma M88 being used in Rafale which India is buying!
It was also flight tested in Russia for good amount of hours...the reason given for its failure was not being able to maintain the required level of thrust during high altitude tests!!
I am surprised or simply don't understand aero-dynamics but was the reason mentioned above the only reason for IAF to not to accept Kaveri for LCA? If so, how it worked out with Rafale then?
Can you please share your expert comments as why the IAF did not accept the Kaveri Engine?
As I was reading about Aero Engines, I got surprised to learn that Kaveri in fact had more thrust (both dry and after-burning!) than even Snecma M88 being used in Rafale which India is buying!
It was also flight tested in Russia for good amount of hours...the reason given for its failure was not being able to maintain the required level of thrust during high altitude tests!!
I am surprised or simply don't understand aero-dynamics but was the reason mentioned above the only reason for IAF to not to accept Kaveri for LCA? If so, how it worked out with Rafale then?