Statements (57)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:Junkers_Jumo_210
|
| gptkbp:aircraft_operated |
gptkb:Junkers_Ju_88
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bore |
150 mm
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:controls |
mechanical throttle
|
| gptkbp:cooling_system |
liquid cooling
water-cooled |
| gptkbp:displacement |
21.0 L
|
| gptkbp:engine |
gptkb:12
V-type aerodynamic efficiency performance upgrades various aircraft types mass production V engine high reliability four-stroke high power-to-weight ratio limited lifespan influenced future designs detailed specifications available performance metrics recorded historically significant engine reflects design philosophy of the era cradle mount context in aviation history contributed to advancements in technology notable characteristics documented operational use in WWII |
| gptkbp:engine_type |
gptkb:Jumo_210_Da
documented specifications available |
| gptkbp:first_flight |
1936
|
| gptkbp:fuel_type |
aviation gasoline
carbureted |
| https://www.w3.org/2000/01/rdf-schema#label |
Jumo 210 H
|
| gptkbp:ignition_system |
spark ignition
|
| gptkbp:is_designed_to |
gptkb:aircraft
|
| gptkbp:is_tested_for |
ground testing
used in various testing facilities |
| gptkbp:maintenance |
moderate maintenance
|
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:notable_feature |
gptkb:engine
|
| gptkbp:performance |
evaluated for performance
|
| gptkbp:power_output |
600 hp
|
| gptkbp:production_location |
produced in multiple facilities
|
| gptkbp:production_years |
1936-1945
|
| gptkbp:propulsion |
variable-pitch propeller
|
| gptkbp:replaced_by |
gptkb:Jumo_213
|
| gptkbp:setting |
liquid-cooled
|
| gptkbp:stroke |
150 mm
|
| gptkbp:successor |
gptkb:Jumo_211
|
| gptkbp:type |
V-12 engine
|
| gptkbp:used_in |
gptkb:Junkers_Ju_87
|
| gptkbp:weight |
400 kg
|