Six Cylinder, Diesel Engine, horizontal, developed 1916, 350hprs
Historical Data:
The Mo 8 was a further developement of the Mo 3 test engine. It's developement was started in spring 1916 at Aachen and construction was finished in summer 1916 at Jumo Magdeburg. A major problem of this test engine was a structural thermal extension, which did not satisfy the Versuchsanstalt at Aachen. Therefore the Mo 8 studies were soon stopped.
Technical Data:
| Engine Designator |
year |
Cyl. |
Bore
in mm |
Stroke
in mm |
Volume
in litres |
Compress.
in % |
length
in m |
Height
in m |
Width
in m |
Weight
in kg |
T/O Power
in kW |
Cruise Power
in kW |
RPM.
|
Fuel
Consump.
g/kWh |
| Mo 8 |
1916 |
6 |
100 |
2 x 150 |
??? |
n.a. |
n.a. |
n.a. |
n.a. |
??? |
257kW / 350 hprs |
n.a. |
100 |
n.a. |
Aircraft Types equipped with Mo 8:
None used in aircraft.
|
