Statements (54)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:controls |
automatic control system
manual throttle control |
| gptkbp:cooling_system |
liquid-cooled
water-cooled ethylene glycol |
| gptkbp:displacement |
38.8 L
|
| gptkbp:emissions_standard |
single exhaust system
|
| gptkbp:engine |
gptkb:12
electric starter developed during WWII detailed specifications available produced in large numbers V-12 configuration performance metrics documented influenced post-war engine designs used in multiple aircraft types Mikulin M-105 cradle mounting system technical data published |
| gptkbp:engine_type |
various variants developed
M-105 R, M-105 PA |
| gptkbp:first_flight |
gptkb:1940
|
| gptkbp:fuel_capacity |
800 mm
1,200 mm 1,800 mm 200 L/h |
| gptkbp:fuel_type |
aviation gasoline
carburetor fuel system |
| https://www.w3.org/2000/01/rdf-schema#label |
M-105 P engine
|
| gptkbp:ignition_system |
spark ignition
|
| gptkbp:is_tested_for |
extensively tested
|
| gptkbp:maintenance |
moderate maintenance requirements
|
| gptkbp:manufacturer |
gptkb:Mikulin
|
| gptkbp:notable_users |
gptkb:Soviet_Air_Force
|
| gptkbp:performance |
high altitude performance
|
| gptkbp:power_output |
1,050 hp
|
| gptkbp:production_years |
1940-1945
|
| gptkbp:propulsion |
variable-pitch propeller
1.75 hp/kg |
| gptkbp:reliability |
high reliability
|
| gptkbp:setting |
V engine
|
| gptkbp:successor |
M-106 engine
|
| gptkbp:torque |
1,200 Nm
flat torque curve pressure lubrication system |
| gptkbp:type |
V-12 piston engine
|
| gptkbp:used_in |
gptkb:Ilyushin_Il-2
|
| gptkbp:weight |
600 kg
|
| gptkbp:bfsParent |
gptkb:Yak-3_U
gptkb:Yak-9_P |
| gptkbp:bfsLayer |
6
|