Statements (26)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:combustionChambers |
1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
2.4 m
|
| gptkbp:engineCycle |
staged combustion
|
| gptkbp:firstFlight |
1987
|
| gptkbp:fuelType |
liquid hydrogen
|
| gptkbp:gimbalRange |
±6°
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-0120
|
| gptkbp:length |
4.5 m
|
| gptkbp:manufacturer |
gptkb:Energomash
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
350 s
455 s |
| gptkbp:status |
retired
|
| gptkbp:successor |
RD-0146
|
| gptkbp:thrustSeaLevel |
1,770 kN
|
| gptkbp:thrustVacuum |
1,961 kN
|
| gptkbp:usedFor |
core stage propulsion
|
| gptkbp:usedIn |
gptkb:Energia_rocket
gptkb:Buran_orbiter |
| gptkbp:weight |
3,500 kg
|
| gptkbp:bfsParent |
gptkb:Energia_rocket
gptkb:Energia_launch_vehicle_program |
| gptkbp:bfsLayer |
6
|