Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:bore |
130 mm
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:configuration |
Liquid-cooled
|
| gptkbp:cooling_system |
Water-cooled
|
| gptkbp:country_of_origin |
gptkb:Germany
|
| gptkbp:displacement |
21.0 L
|
| gptkbp:engine_configuration |
V engine
|
| gptkbp:first_flight |
1936
|
| gptkbp:fuel_type |
Benzin
|
| https://www.w3.org/2000/01/rdf-schema#label |
Jumo 210 B
|
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:power_output |
600 hp
700 hp |
| gptkbp:production_years |
1936-1940
|
| gptkbp:stroke |
150 mm
|
| gptkbp:successor |
gptkb:Jumo_211
|
| gptkbp:type |
V-12 engine
|
| gptkbp:used_in |
gptkb:Junkers_Ju_87_Stuka
gptkb:Junkers_Ju_87 |
| gptkbp:valve_configuration |
Overhead valves
|
| gptkbp:weight |
400 kg
|