| Snecma Atar ✕ | |
|---|---|
| Aircraft Engine Manufacturer | ATAR |
| Aircraft Engine Type | Turbojet |
| Dry Weight (kg) | 1456 |
| Diameter (mm) | 1000 |
| Length (mm) | 5900 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Snecma_Atar |
| Geared Fan | No |
| Combustion Chamber | annular |
| Afterburner | Yes |
| Streams | 1 |
| Maximum Takeoff Thrust (kN) | 42 |
| Thrust To Weight | 2.94 |
| Specific Fuel Consumption (g/(kN·s)) | 2917.475 |
| Compressor Description | 9-stage axial compressor |
| Turbine Description | Two-stage |