|
gptkbp:instanceOf
|
piston engine
|
|
gptkbp:burnTime
|
253 seconds
|
|
gptkbp:combustionChambers
|
2
|
|
gptkbp:countryOfOrigin
|
gptkb:Russia
|
|
gptkbp:cycle
|
staged combustion
|
|
gptkbp:derivedFrom
|
gptkb:RD-170_engine
|
|
gptkbp:diameter
|
3.15 m
|
|
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 engine
|
|
gptkbp:length
|
3.56 m
|
|
gptkbp:manufacturer
|
gptkb:NPO_Energomash
|
|
gptkbp:nozzleExpansionRatio
|
36
|
|
gptkbp:oxidizer
|
liquid oxygen
|
|
gptkbp:propulsion
|
gptkb:water
|
|
gptkbp:specificImpulseVacuum
|
311 s
338 s
|
|
gptkbp:status
|
in production
|
|
gptkbp:throttleCapability
|
fixed
|
|
gptkbp:thrustSeaLevel
|
3827 kN
|
|
gptkbp:thrustVacuum
|
4152 kN
|
|
gptkbp:totalProduced
|
since 1999
|
|
gptkbp:usedBy
|
gptkb:United_Launch_Alliance
|
|
gptkbp:usedFor
|
launch vehicle first stage
|
|
gptkbp:usedIn
|
gptkb:Atlas_V
gptkb:Atlas_III
gptkb:Atlas_V_551
gptkb:Atlas_V_401
gptkb:Atlas_V_N22
|
|
gptkbp:weight
|
5480 kg
|
|
gptkbp:bfsParent
|
gptkb:Energomash
gptkb:RD-170_engine
|
|
gptkbp:bfsLayer
|
6
|