Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:combustionChambers |
4
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:cycle |
staged combustion
|
| gptkbp:diameter |
3.55 m
|
| gptkbp:firstFlight |
1985
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:gimbalRange |
±8°
|
| gptkbp:length |
3.8 m
|
| gptkbp:manufacturer |
gptkb:NPO_Energomash
|
| gptkbp:notableDerivative |
gptkb:RD-171
gptkb:RD-191 gptkb:RD-180 |
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
337 s
309 s |
| gptkbp:status |
in production
|
| gptkbp:thrustSeaLevel |
7,257 kN
|
| gptkbp:thrustVacuum |
7,903 kN
|
| gptkbp:usedBy |
gptkb:Soviet_space_program
gptkb:Russian_space_program |
| gptkbp:usedIn |
gptkb:Energia_rocket
gptkb:Zenit_rocket |
| gptkbp:weight |
9,750 kg
|
| gptkbp:bfsParent |
gptkb:NPO_Energomash
gptkb:Glushko_Design_Bureau |
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-170 rocket engine
|