Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:Junkers_Ju_388
gptkb:Ju_88_G |
| gptkbp:aircraft_operated |
heavy fighters
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bore |
150 mm
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:cooling_system |
gptkb:fandom
liquid cooling liquid-cooled |
| gptkbp:displacement |
35.7 L
|
| gptkbp:engine |
gptkb:aircraft
gptkb:battle high performance mass production high reliability high power output V configuration military specifications developed during WWII used in various aircraft models significant in aviation history produced in large quantities supercharged advanced technology for its time influenced post-war designs V12 configuration good efficiency V12 layout powerful and efficient V12 engine configuration Jumo 210/211/213 Junkers design developed by Junkers incorporated advanced engineering principles operational in WWII |
| gptkbp:engine_type |
piston engine
Jumo 213 A, Jumo 213 E, Jumo 213 F |
| gptkbp:first_flight |
gptkb:1942
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Junkers Jumo 213
|
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:notable_users |
gptkb:Luftwaffe
|
| gptkbp:power_output |
1,800 hp
|
| gptkbp:production_years |
1942-1945
|
| gptkbp:propulsion |
2.25 hp/kg
|
| gptkbp:setting |
gptkb:V12
|
| gptkbp:stroke |
150 mm
|
| gptkbp:successor |
gptkb:Jumo_222
|
| gptkbp:type |
liquid-cooled V12 engine
|
| gptkbp:used_in |
gptkb:star
gptkb:Messerschmitt_Me_262 |
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
about 800 kg
|