| Aircraft Engine Manufacturer |
Turbomeca |
BMW |
| Aircraft Engine Type |
Turbojet |
Rocket |
| Dry Weight (kg) |
115 |
160 |
| Diameter (mm) |
405 |
1250 |
| Length (mm) |
1361 |
2400 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Turbomeca_Arbizon |
en.wikipedia.org/wiki/BMW_109-558 |
| Fuel |
|
R-Stoff fuel (50% triethylamine and 50% xylidine) and SV-Stoff oxidiser (94% nitric acid with 6% dinitrogen tetroxide) |
| Geared Fan |
No |
No |
| Combustion Chamber |
|
Hypergolic combustion in a single combustion chamber |
| Afterburner |
No |
No |
| Streams |
1 |
1 |
| Maximum Takeoff Thrust (kN) |
3.73 |
3.7 |
| Thrust To Weight |
3.31 |
0.0231 |
| Compressor Description |
single-stage axial, single-stage centrifugal |
|
| Turbine Description |
single-stage |
|