|
gptkbp:instanceOf
|
turboprop engine
|
|
gptkbp:application
|
military aircraft
passenger aircraft
cargo_aircraft
|
|
gptkbp:compressionRatio
|
8:1
|
|
gptkbp:controls
|
hydromechanical
|
|
gptkbp:coolingSystem
|
air-cooled
forced air
|
|
gptkbp:diameter
|
1,100 mm
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissionsStandard
|
ICAO_Chapter_3
|
|
gptkbp:engine
|
inline
|
|
gptkbp:engineType
|
turboprop
AI-20M-1
AI-20M-2
AI-20M-3
AI-20M-4
AI-20M-5
|
|
gptkbp:exhaustSystem
|
single exhaust
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:fuel_capacity
|
annular
0.5 kg/kW·h
|
|
gptkbp:fuelType
|
spark ignition
kerosene
dual fuel system
|
|
gptkbp:hasArea
|
flight testing
ground testing
Soviet_certification
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Ivchenko AI-20M
|
|
gptkbp:inspiration
|
gptkb:Soviet_Union
|
|
gptkbp:is_used_in
|
gptkb:Tupolev_Tu-95
gptkb:Antonov_An-12
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
Ivchenko
|
|
gptkbp:noise_level
|
85 dB
|
|
gptkbp:operational_status
|
civil aviation
|
|
gptkbp:operationalHistory
|
used_in_Soviet_Union
|
|
gptkbp:operationalRange
|
1,500 km
|
|
gptkbp:performances
|
5,000 hours
|
|
gptkbp:powerOutput
|
2,950 kW
|
|
gptkbp:productionYears
|
1950s
|
|
gptkbp:propulsion
|
4
8:1
variable-pitch
4,000 lbf
|
|
gptkbp:related_engine
|
AI-14
AI-24
Brayton_cycle
|
|
gptkbp:retirementYear
|
1990s
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:setting
|
two-shaft
|
|
gptkbp:successor
|
gptkb:AI-20D
|
|
gptkbp:weight
|
500 kg
|