|
gptkbp:instanceOf
|
rocket engine
|
|
gptkbp:barrelLength
|
69 bar
|
|
gptkbp:chemicalFormula
|
liquid oxygen
|
|
gptkbp:developer
|
2002
|
|
gptkbp:documentType
|
bell nozzle
|
|
gptkbp:engine
|
1 to 9
|
|
gptkbp:engineType
|
gptkb:Merlin_Vacuum
gptkb:Merlin_1A
Merlin 1B
Merlin 1C
Merlin 2
|
|
gptkbp:firstFlight
|
March 24, 2006
|
|
gptkbp:fuel_capacity
|
single chamber
|
|
gptkbp:fuelType
|
RP-1
spark plug
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Merlin engine
|
|
gptkbp:is_designed_to
|
gptkb:SpaceX
|
|
gptkbp:is_used_in
|
gptkb:Falcon_1
gptkb:Falcon_9
gptkb:Falcon_Heavy
|
|
gptkbp:launchSite
|
gptkb:Kennedy_Space_Center
gptkb:Cape_Canaveral_Space_Force_Station
|
|
gptkbp:missions
|
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:noise_level
|
311 seconds
282 seconds
|
|
gptkbp:number_of_stages
|
gptkb:Merlin_Vacuum
gptkb:Falcon_9_first_stage
|
|
gptkbp:operational_status
|
active
|
|
gptkbp:propulsion
|
845 kN
|
|
gptkbp:related_engine
|
gas-generator cycle
|
|
gptkbp:reliability
|
true
|
|
gptkbp:setting
|
single or clustered
|
|
gptkbp:successor
|
Raptor engine
|
|
gptkbp:type
|
liquid rocket engine
|
|
gptkbp:weight
|
450 kg
|