Statements (54)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Albatros_D._III
gptkb:Albatros_D._V gptkb:Fokker_E._III |
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bore |
150 mm
|
| gptkbp:compression_ratio |
5.5:1
|
| gptkbp:cooling_system |
liquid-cooled
water-cooled |
| gptkbp:displacement |
14.6 L
|
| gptkbp:engine |
high reliability
high power-to-weight ratio inline inline engine detailed specifications available used in various aircraft models straight-six significant in aviation history dual ignition approximately 1,000 hours performance metrics documented influenced future aircraft engine designs six-cylinder produced in limited quantities incorporated advanced technologies for its time characterized by smooth operation developed during WWI contributed to German aviation efforts maximum RPM 1,800 |
| gptkbp:engine_type |
D. II Ia, D. II Ib
|
| gptkbp:first_flight |
gptkb:1917
|
| gptkbp:fuel_type |
gptkb:product
aviation gasoline |
| https://www.w3.org/2000/01/rdf-schema#label |
Mercedes D. III
|
| gptkbp:ignition_system |
magneto
|
| gptkbp:is_tested_for |
extensively tested before production
tested at Mercedes facilities |
| gptkbp:maintenance |
moderate maintenance required
|
| gptkbp:manufacturer |
gptkb:Mercedes
|
| gptkbp:notable_users |
gptkb:German_Air_Force
|
| gptkbp:operational_history |
gptkb:World_War_I
|
| gptkbp:power_output |
160 hp
|
| gptkbp:production_years |
1917-1918
|
| gptkbp:propulsion |
fixed-pitch
|
| gptkbp:replaced_by |
gptkb:Mercedes_D._IV
|
| gptkbp:setting |
liquid-cooled
|
| gptkbp:stroke |
200 mm
|
| gptkbp:successor |
Mercedes D. II Ia
|
| gptkbp:torque |
high torque
|
| gptkbp:type |
inline six-cylinder engine
|
| gptkbp:used_in |
gptkb:Fokker_D._VII
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
200 kg
|