Statements (47)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:Junkers_A_340
gptkb:Junkers_A_380 |
| gptkbp:aircraft_operated |
gptkb:Junkers_CL._I
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:cooling_system |
gptkb:fandom
liquid cooling water-cooled |
| gptkbp:design |
Junkers design team
|
| gptkbp:displacement |
4.0 L
4000 cubic centimeters |
| gptkbp:engine |
8
post-World War I V8 configuration innovative for its time 150 horsepower considered reliable for its time V8 arrangement V8 layout developed during the early aviation era. good performance for early aircraft produced in Germany used in several early aircraft models |
| gptkbp:engine_type |
reciprocating engine
|
| gptkbp:fuel_capacity |
200 kilograms
|
| gptkbp:fuel_type |
gptkb:product
aviation gasoline runs on aviation gasoline |
| gptkbp:historical_significance |
early aviation engine development
|
| https://www.w3.org/2000/01/rdf-schema#label |
Junkers L5 engine
|
| gptkbp:ignition_system |
magneto ignition
uses magneto ignition system |
| gptkbp:is_designed_to |
aircraft propulsion
|
| gptkbp:manufacturer |
gptkb:Junkers
|
| gptkbp:original_run |
1919
|
| gptkbp:power_output |
150 hp
|
| gptkbp:production_years |
1919-1925
|
| gptkbp:setting |
V engine
|
| gptkbp:successor |
gptkb:Junkers_L8_engine
|
| gptkbp:torque |
300 Nm
300 Newton-meters |
| gptkbp:type |
liquid-cooled V8 engine
|
| gptkbp:used_in |
gptkb:Junkers_F.13
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
200 kg
|