| BMW 109-718 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | BMW |
| Aircraft Engine Type | Rocket |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/BMW_109-718 |
| Fuel | Diesel fuel and red fuming nitric acid (RFNA / S-Stoff) oxidiser with injected catalyst or R-stoff / SV-stoff fuel and … |
| Geared Fan | No |
| Combustion Chamber | Catalyst ignited or Hypergolic combustion in a single combustion chamber |
| Afterburner | No |
| Streams | 1 |
| Maximum Takeoff Thrust (kN) | 12.2625 |
| Specific Fuel Consumption (g/(kN·s)) | 15.89 |