Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.45 m
|
| gptkbp:engineCycle |
staged combustion
|
| gptkbp:exportedTo |
gptkb:India
|
| gptkbp:firstFlight |
1985
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:gimbalRange |
±6°
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-120
|
| gptkbp:length |
3.55 m
|
| gptkbp:manufacturer |
gptkb:NPO_Energomash
|
| gptkbp:notableDerivative |
gptkb:RD-170
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
350 s
297 s |
| gptkbp:status |
in production
|
| gptkbp:thrustSeaLevel |
682 kN
|
| gptkbp:thrustVacuum |
833 kN
|
| gptkbp:usedIn |
gptkb:Zenit_rocket
gptkb:Indian_SCE-200_engine_(derivative) gptkb:Mayak_launch_vehicle |
| gptkbp:weight |
1125 kg
|
| gptkbp:bfsParent |
gptkb:Zenit_rocket
|
| gptkbp:bfsLayer |
6
|