| Aircraft Engine Manufacturer |
Argus Motoren |
BMW |
| Aircraft Engine Type |
Pulsejet |
Rocket |
| Dry Weight (kg) |
170 |
160 |
| Diameter (mm) |
546.1 |
1250 |
| Length (mm) |
3657.6 |
2400 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Argus_As_014 |
en.wikipedia.org/wiki/BMW_109-558 |
| Fuel |
Gasoline |
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) |
3.53 |
3.7 |
| Thrust To Weight |
2.12 |
0.0231 |
| Compressor Description |
None, compression was achieved acoustically, with additional ram pressure when in flight. |
|