Re: ADA LCA Tejas Mark-II
A Comparison is required >>
General Electric F404
Length: 154 in (3,912 mm)
Diameter: 35 in (889 mm)
Dry weight: 2,282 lb (
1,036 kg)
Dry thrust: 11,000 lbf (48.9 kN) military thrust
With AfterBurners : 17,700 lbf (78.7 kN) with afterburner
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GTRE Kaveri
Length: 137.4 in (3490 mm)
Diameter: 35.8 in (910 mm)
Dry weight: 2,724 lb (
1,235 kg)
[Goal: 2,100-2450 lb (950-1100 kg)]
Military thrust : 11,687 lbf (52.0 kN)
Full afterburner: 18,210 lbf (81.0 kN)
(planned to be refined to >95 kN)
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Dr. V.K. Saraswat talk in IITB >>
- Current Kaveri
generates 78KN wet thrust Vs goal of 81KN.
- Higher turbine inlet temp 1900 deg K, requires SCB
- HAL has SCB tech from Su-30 ToT,
but HAL doesn't have knowledge to create SCB for new configuration reqd by new Kaveri. HAL personnel lack knowledge for creating new design.
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Conclusion >
In present config, Kaveri is over-weighted, IAF needed weight reduction or Max thrust 81kn, Though IMHO, Kaveri is good enough to mass produce for Tejas which are intended for export as many nation does not want to have US made engines, It is also applicable for MIG-21/27 class fighters both in service and export,
Once it get its certifications ..
Next year, the GTRE plans to show the engine's performance first on an Il-76 plane and
then as the second engine fitted on a twin-engined fighter like MiG-29. It would be tuned to certification standards >>
New tailwinds for Kaveri engine - The Hindu
Has anyone so far compared the performance of Tejas with latest Kaveri engine and that with GE Engine? What áre the limitations of Tejas with Kaveri engine? How much thrust is IAF expecting and how much has been achieved by Kaveri? I see many conflicting reports and that is why I am requesting to share a final accepted version of the report.