| Standard thrust | 20-23 kg ±1 |
| Fuel consumption | 524 g/min |
| Weight | 4 kg |
| Diameter | 130 mm |
| Length | 330 mm ±2 |
| Idle speed | 46000 rpm |
| Maximum speed | 108000 rpm |
| Exhaust gas temperature | 950°C |
| Maximum use altitude | 10000 m |
| Power used | 3S LIPO 25C and above |
| Fuel | aviation kerosene |
| Use of lubricating oil | adding 3%-5% Pegasus No. 2 oil to kerosene |
| Service life | 25 hours |
| Ambient temperature during operation | -25 to 50°C |