Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:configuration |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designer |
gptkb:Alexander_Mikulin
|
| gptkbp:diameter |
1.3 m
|
| gptkbp:enteredService |
1952
|
| gptkbp:firstFlight |
1948
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
5.2 m
|
| gptkbp:manufacturer |
gptkb:Mikulin_Design_Bureau
|
| gptkbp:numberOfStages |
2
8 |
| gptkbp:successor |
gptkb:Kuznetsov_NK-8
|
| gptkbp:thrust |
8,700 kgf
|
| gptkbp:usedInAircraft |
gptkb:Tupolev_Tu-104
gptkb:Tupolev_Tu-16 gptkb:Myasishchev_M-4 |
| gptkbp:weight |
2,350 kg
|
| gptkbp:bfsParent |
gptkb:Tupolev_Tu-104
gptkb:Tu-104 |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Mikulin AM-3 turbojet
|