Statements (58)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:La-15_fighter_aircraft
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bore |
150 mm
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:cooling_system |
liquid-cooled
water-cooled uses water for cooling |
| gptkbp:displacement |
45 liters
|
| gptkbp:engine |
gptkb:12
gptkb:battle limited production high reliability four-stroke high power-to-weight ratio inline bombers V configuration influenced future designs detailed technical specifications liquid-cooled V12 measured in horsepower Mikulin AM-38 powerful and efficient incorporated new technologies of the era served in various military conflicts developed in post-war era known for reliability in service part of Soviet aviation history produced in the Soviet Union features advanced engineering for its time developed by a team of engineers at Mikulin faced production challenges during early years focused on performance and durability influenced the aircraft engine market in the USSR operated in various aircraft models significant in the development of Soviet aviation engines |
| gptkbp:engine_type |
reciprocating engine
AM-5 A |
| gptkbp:first_flight |
1947
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mikulin AM-5
|
| gptkbp:ignition_system |
spark ignition
|
| gptkbp:is_tested_for |
extensive ground testing
tested in specialized aviation facilities. |
| gptkbp:manufacturer |
gptkb:Mikulin
|
| gptkbp:notable_users |
gptkb:Soviet_Air_Force
|
| gptkbp:origin |
gptkb:Monarch
|
| gptkbp:power_output |
1,700 hp
|
| gptkbp:production_years |
1947-1950
|
| gptkbp:setting |
V engine
|
| gptkbp:stroke |
150 mm
|
| gptkbp:successor |
Mikulin AM-9
|
| gptkbp:type |
V12 piston engine
|
| gptkbp:used_in |
gptkb:Tupolev_Tu-4
|
| gptkbp:valve_configuration |
overhead valve
|
| gptkbp:weight |
600 kg
|