Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:chamberPressure |
26.7 MPa
|
| gptkbp:combustionChambers |
2
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:cycle |
staged combustion
|
| gptkbp:derivedFrom |
gptkb:RD-170
|
| gptkbp:diameter |
2.58 m
|
| gptkbp:engineType |
liquid bipropellant
|
| gptkbp:exportedTo |
gptkb:United_States
|
| gptkbp:firstFlight |
2000
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:gimbalRange |
8 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-180
|
| gptkbp:length |
3.56 m
|
| gptkbp:manufacturer |
gptkb:NPO_Energomash
|
| gptkbp:nozzleExpansionRatio |
36
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:reusable |
no
|
| gptkbp:specificImpulseVacuum |
311 s
338 s |
| gptkbp:status |
in production
|
| gptkbp:throttleable |
no
|
| gptkbp:thrustSeaLevel |
3827 kN
|
| gptkbp:thrustVacuum |
4152 kN
|
| gptkbp:usedBy |
gptkb:United_Launch_Alliance
|
| gptkbp:usedFor |
launch vehicles
|
| gptkbp:usedIn |
gptkb:Atlas_V
gptkb:Atlas_III |
| gptkbp:weight |
5480 kg
|
| gptkbp:bfsParent |
gptkb:Atlas_V
gptkb:Atlas_V_411 |
| gptkbp:bfsLayer |
5
|