Designed to power modern supersonic trainers, training-combat and light combat aircraft operated at moderate supersonic speeds (up to M=1.6). Installed on the L-15B.
Full afterburning power (SLS, ISA) | |
Thrust, kgf | 4,200 |
Specific fuel consumption, kg/h/kgf | 1,9 |
Full afterburning power (H=11,000 m, М=1,4; ISA, σin=0,97) | |
Thrust, kgf | 2 760 |
Maximum (SLS, ISA) | |
Thrust, kgf | 2,500 |
Specific fuel consumption, kg/kgf/h | 0,66 |
Dimensions (without inlet fairing), mm | 3,138 х 863 х 1,142 |
Weight, dry, kg | 560 |