|
gptkbp:instanceOf
|
rocket engine
|
|
gptkbp:barrelLength
|
69 bar
|
|
gptkbp:chemicalFormula
|
liquid oxygen
|
|
gptkbp:coolingSystem
|
film cooling
|
|
gptkbp:designedBy
|
gptkb:SpaceX
|
|
gptkbp:developer
|
2002
|
|
gptkbp:diameter
|
1.1 m
|
|
gptkbp:firstAwarded
|
gptkb:Falcon_9_first_stage
|
|
gptkbp:firstFlight
|
2006
|
|
gptkbp:firstMatch
|
gptkb:Falcon_9_second_stage
|
|
gptkbp:fuelType
|
RP-1
staged combustion
|
|
gptkbp:hasContent
|
282 seconds (sea level)
311 seconds (vacuum)
|
|
gptkbp:hasVersion
|
5
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
merlin engine
|
|
gptkbp:length
|
3.1 m
|
|
gptkbp:notableFeature
|
CRS-1
CRS-20
CRS-10
CRS-12
CRS-15
CRS-16
CRS-17
CRS-18
CRS-19
CRS-21
CRS-22
CRS-23
CRS-24
CRS-26
CRS-27
CRS-28
CRS-29
CRS-3
CRS-30
CRS-4
CRS-5
CRS-6
CRS-7
CRS-9
CRS-2
CRS-11
CRS-13
CRS-14
CRS-25
CRS-8
|
|
gptkbp:numberOfEpisodes
|
1 to 9
|
|
gptkbp:propulsion
|
845 kN
|
|
gptkbp:related_engine
|
gas-generator cycle
|
|
gptkbp:reliability
|
yes
|
|
gptkbp:status
|
in production
|
|
gptkbp:successor
|
Raptor engine
|
|
gptkbp:type
|
liquid rocket engine
|
|
gptkbp:usedIn
|
gptkb:Falcon_1
gptkb:Falcon_9
gptkb:Falcon_Heavy
|
|
gptkbp:weight
|
450 kg
|