Statements (50)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turboprop engine
|
| gptkbp:application |
military aircraft
passenger aircraft cargo_aircraft |
| gptkbp:compressionRatio |
8:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
1,100 mm
|
| gptkbp:engineType |
gptkb:AI-20J
gptkb:AI-20Q gptkb:AI-20M gptkb:AI-20F gptkb:AI-20D gptkb:AI-20R turboprop AI-20K AI-20A AI-20B AI-20E AI-20G AI-20H AI-20L AI-20N AI-20O AI-20P AI-20V AI-20Y AI-20Z AI-20S AI-20T AI-20U AI-20X |
| gptkbp:firstFlight |
1955
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ivchenko AI-20D
|
| gptkbp:is_used_in |
gptkb:Tupolev_Tu-95
gptkb:Antonov_An-12 |
| gptkbp:length |
1,800 mm
|
| gptkbp:manufacturer |
Ivchenko
|
| gptkbp:notableUsers |
gptkb:Egyptian_Air_Force
gptkb:Soviet_Air_Force gptkb:Indian_Air_Force gptkb:Cuban_Air_Force Aeroflot |
| gptkbp:operationalHistory |
gptkb:Soviet_Union
gptkb:Ukraine |
| gptkbp:powerOutput |
2,950 kW
|
| gptkbp:propulsion |
4,000 lbf
|
| gptkbp:related_engine |
Brayton_cycle
|
| gptkbp:setting |
two-shaft
|
| gptkbp:weight |
500 kg
|