Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:cycle |
staged combustion
|
| gptkbp:diameter |
1.8 m
|
| gptkbp:firstFlight |
1967
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
NK-15
|
| gptkbp:length |
3.7 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
297 s
331 s |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:NK-33
|
| gptkbp:thrustSeaLevel |
1,505 kN
|
| gptkbp:thrustVacuum |
1,753 kN
|
| gptkbp:usedIn |
gptkb:N1_rocket
gptkb:N1_first_stage |
| gptkbp:bfsParent |
gptkb:N1_rocket
|
| gptkbp:bfsLayer |
6
|