Argus Panoptes
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why is jf-17 considered under powered when its engine thrust is exactly similar to gripen C and earliest version of mirage2000.? while its T/W better than both..i mean under in avionics may be but why raw engine thrust?
MIRAGE2000
M53-5 - powered initial Mirage 2000C models [1]
Dry thrust: 54.0 kN (5,500 kgp / 12,230 lbf)
Afterburning thrust: 86.3 kN (8,800 kgp / 19,400 lbf)
M53-P2 - powered later Mirage 2000C models and used to upgrade earlier models [2]
Dry thrust: 64.7 kN (6,600 kgp / 14,500 lbf)
Afterburning thrust: 95.1 kN (9,700 kgp / 21,400 lbf)
gripen C
Powerplant: 1 × Volvo Aero RM12 afterburning turbofan/ General Electric F404
Dry thrust: 54 kN (12,100 lbf)
Thrust with afterburner: 80.5 kN (18,100 lbf)
JF-17
Powerplant: 1 × Klimov RD-93
Dry thrust: 49.4 kN[19] / 51.2 kN (11,106 lbf / 11,510 lbf)
Thrust with afterburner: 84.5 kN (19,000 lbf)
NOTE I HAVE USED THE LOWEST FIGURES FOR RD-93
T/W is higher simply because empty weight and loaded weight of JF-17 much lower..
every body keeps mentioning how under powered JF-17 is but never heard an answer to this argument..if JF-17 is under powered than why isnt the gripen C considered under powered?
The empty and loaded weights of the JF-17 are more than the Gripen C:
JF-17: 14,500 lbs empty, 20,000 lbs loaded.
Gripen C: 12,600 lbs empty, 18,700 lbs loaded.
The Gripen is considered underpowered too, but not by as much as the JF-17. Anything under unity is relatively underpowered for a front line combat role.