| Aircraft Engine Manufacturer |
BMW |
TEM (Turbine Engine Manufacturing) |
| Aircraft Engine Type |
Rocket |
Turbojet |
| Dry Weight (kg) |
160 |
54.7 |
| Diameter (mm) |
1250 |
|
| Length (mm) |
2400 |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/BMW_109-558 |
en.wikipedia.org/wiki/TEM_Toloue-4 |
| 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) |
3.7 |
3.7 |
| Thrust To Weight |
0.0231 |
|