Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:chamber |
1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:cycle |
staged combustion
|
| gptkbp:diameter |
2.4 m
|
| gptkbp:firstFlight |
1985
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:gimbalRange |
6 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-118
|
| gptkbp:length |
3.6 m
|
| gptkbp:manufacturer |
gptkb:Energomash
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
311 s
350 s |
| gptkbp:status |
retired
|
| gptkbp:successor |
gptkb:RD-120
|
| gptkbp:thrustSeaLevel |
833 kN
|
| gptkbp:thrustVacuum |
981 kN
|
| gptkbp:usedIn |
gptkb:Zenit_rocket
|
| gptkbp:usedOnStage |
second stage
|
| gptkbp:weight |
1,125 kg
|
| gptkbp:bfsParent |
gptkb:RD-108
gptkb:RD-108_rocket_engine |
| gptkbp:bfsLayer |
8
|