Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Antonov_An-72
gptkb:Antonov_An-74 gptkb:Beriev_Be-200 gptkb:Yakovlev_Yak-42 |
| gptkbp:bypassRatio |
5.7:1
|
| gptkbp:combustorType |
annular
|
| gptkbp:compressionRatio |
seven-stage high-pressure compressor
six-stage low-pressure compressor three-stage fan |
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.46 m
|
| gptkbp:firstFlight |
1971
|
| https://www.w3.org/2000/01/rdf-schema#label |
D-36 turbofan
|
| gptkbp:introduced |
1974
|
| gptkbp:length |
3.95 m
|
| gptkbp:manufacturer |
gptkb:Motor_Sich
gptkb:Ivchenko-Progress |
| gptkbp:successor |
gptkb:Progress_D-436
|
| gptkbp:thrust |
63 kN
|
| gptkbp:turbineType |
four-stage low-pressure turbine
two-stage high-pressure turbine |
| gptkbp:usedIn |
gptkb:aircraft
civil aviation |
| gptkbp:weight |
1,450 kg
|
| gptkbp:bfsParent |
gptkb:An-74-200
|
| gptkbp:bfsLayer |
7
|