Statements (55)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Junkers_Jumo_211
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bore |
150 mm
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:controls |
Throttle control
|
| gptkbp:cooling_system |
Liquid-cooled
Water-cooled |
| gptkbp:displacement |
33.9 L
|
| gptkbp:engine |
gptkb:V12
Various aircraft types Electric start Used in various military operations Single-stage supercharger Detailed specifications available Significant historical impact Nose-mounted Recognized for its engineering excellence Advanced features for its time Developed in the late 1930s High performance for military applications Influenced post-war engine designs Introduced several innovations in design Limited by technology of the time Specifications published in technical manuals Widely used during its era |
| gptkbp:engine_type |
Multiple variants developed
|
| gptkbp:first_flight |
1938
|
| gptkbp:fuel_type |
Benzin
Direct fuel injection |
| https://www.w3.org/2000/01/rdf-schema#label |
Jumo 211 F
|
| gptkbp:ignition_system |
Magneto ignition
|
| gptkbp:impact |
Had a significant impact on aviation technology.
|
| gptkbp:is_tested_for |
Extensive testing during development
|
| gptkbp:maintenance |
Moderate maintenance requirements
|
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:operational_history |
gptkb:World_War_II
|
| gptkbp:performance |
Good performance at altitude
|
| gptkbp:power_output |
1,200 hp
|
| gptkbp:produced_by |
Over 30,000
|
| gptkbp:production_years |
1938-1945
|
| gptkbp:reliability |
High reliability
|
| gptkbp:setting |
V engine
|
| gptkbp:stroke |
150 mm
|
| gptkbp:successor |
gptkb:Jumo_213
|
| gptkbp:tuning |
Adjustable tuning
|
| gptkbp:type |
V12 piston engine
|
| gptkbp:used_in |
gptkb:Junkers_Ju_88
gptkb:Junkers_Ju_87_Stuka |
| gptkbp:valve_configuration |
Overhead valve
|
| gptkbp:variant |
gptkb:Jumo_211_A
gptkb:Jumo_211_J Jumo 211 R |
| gptkbp:weight |
450 kg
|