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 |
Applicability
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L-15B