Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:burnTime |
253 s
|
| gptkbp:chamber |
2
|
| gptkbp:countryOfOrigin |
gptkb:Russia
|
| gptkbp:cycle |
staged combustion
|
| gptkbp:derivedFrom |
gptkb:RD-170
|
| gptkbp:diameter |
2.58 m
|
| gptkbp:firstFlight |
2000
|
| gptkbp:fuelType |
gptkb:RP-1
|
| gptkbp:gimbalRange |
8 degrees
|
| https://www.w3.org/2000/01/rdf-schema#label |
RD-180 (first stage)
|
| gptkbp:length |
3.56 m
|
| gptkbp:manufacturer |
gptkb:NPO_Energomash
|
| gptkbp:nozzleCount |
1
|
| gptkbp:oxidizer |
liquid oxygen
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:specificImpulseVacuum |
311 s
338 s |
| gptkbp:status |
in service
|
| gptkbp:thrustSeaLevel |
3827 kN
|
| gptkbp:thrustVacuum |
4152 kN
|
| gptkbp:usedBy |
gptkb:Lockheed_Martin
gptkb:United_Launch_Alliance |
| gptkbp:usedFor |
launch vehicles
|
| gptkbp:usedIn |
gptkb:Atlas_V
|
| gptkbp:weight |
5480 kg
|
| gptkbp:bfsParent |
gptkb:Atlas_V_541
|
| gptkbp:bfsLayer |
6
|