Statements (53)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compression_ratio |
16:1
|
| gptkbp:cooling_system |
liquid-cooled
water-cooled |
| gptkbp:displacement |
20.7 L
|
| gptkbp:engine |
gptkb:12
gptkb:Jumo_200_series various aircraft types V engine high reliability four-stroke V configuration high torque long lifespan high thermal efficiency inline engine detailed specifications available incorporated several innovations produced in large numbers significant in aviation history advanced technology for its time performance metrics documented developed during the late 1930s 2000 RPM legacy in diesel engine development notable characteristics include durability |
| gptkbp:engine_type |
multiple variants available
|
| gptkbp:first_flight |
1939
|
| gptkbp:fuel_type |
diesel
direct injection |
| gptkbp:horsepower |
0.67 kg/hp
|
| https://www.w3.org/2000/01/rdf-schema#label |
Jumo 207
|
| gptkbp:ignition_system |
compression ignition
|
| gptkbp:is_tested_for |
extensively tested
tested in specialized facilities |
| gptkbp:maintenance |
moderate maintenance requirements
|
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:noise_level |
moderate noise level
|
| gptkbp:notable_users |
gptkb:Luftwaffe
|
| gptkbp:operational_history |
gptkb:World_War_II
|
| gptkbp:power_output |
600 hp
|
| gptkbp:production_years |
1939-1945
|
| gptkbp:setting |
gptkb:V12
|
| gptkbp:successor |
gptkb:Jumo_210
|
| gptkbp:torque |
high torque output
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:Junkers_Ju_87
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
400 kg
|
| gptkbp:bfsParent |
gptkb:Jumo_205_D
gptkb:Junkers_Jumo_205 |
| gptkbp:bfsLayer |
7
|