Statements (28)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:combustionChambers |
1
|
gptkbp:countryOfOrigin |
gptkb:Russia
|
gptkbp:diameter |
2.1 m
|
gptkbp:engineCycle |
oxidizer-rich staged combustion
|
gptkbp:firstFlight |
2014
|
gptkbp:fuelType |
kerosene
|
gptkbp:gimbalRange |
+/- 8 degrees
|
https://www.w3.org/2000/01/rdf-schema#label |
RD-191 engine
|
gptkbp:length |
3.6 m
|
gptkbp:manufacturer |
gptkb:NPO_Energomash
|
gptkbp:notableDerivative |
gptkb:RD-170_engine
|
gptkbp:oxidizer |
liquid oxygen
|
gptkbp:predecessor |
gptkb:RD-170_engine
|
gptkbp:propulsion |
gptkb:water
|
gptkbp:specificImpulseVacuum |
311 s
337 s |
gptkbp:status |
in production
|
gptkbp:successor |
gptkb:RD-193_engine
|
gptkbp:throttleRange |
27% to 105%
|
gptkbp:thrustSeaLevel |
1900 kN
|
gptkbp:thrustVacuum |
2120 kN
|
gptkbp:usedIn |
gptkb:Angara_rocket
gptkb:Baikal_booster |
gptkbp:weight |
2320 kg
|
gptkbp:bfsParent |
gptkb:Energomash
gptkb:RD-170_engine |
gptkbp:bfsLayer |
6
|