|
gptkbp:instance_of
|
gptkb:rocket
|
|
gptkbp:bfsLayer
|
4
|
|
gptkbp:bfsParent
|
gptkb:Merlin_engines
gptkb:RD-0110_engine
gptkb:RD-107_engine
gptkb:F-1_engines
gptkb:Rocketdyne_F-1
gptkb:RD-108_engine
gptkb:Merlin_engine
gptkb:F-1_engine
gptkb:BE-4
gptkb:Aerojet_Rocketdyne_engines
|
|
gptkbp:can_be_used_with
|
gptkb:LOX
liquid oxygen
|
|
gptkbp:developed_by
|
gptkb:Aerojet_Rocketdyne
kerosene
refined petroleum
|
|
gptkbp:financial_performance
|
room temperature
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RP-1
|
|
gptkbp:is_a
|
kerosene
|
|
gptkbp:is_compared_to
|
hydrazine
liquid hydrogen
|
|
gptkbp:is_compatible_with
|
aluminum
RP-2
|
|
gptkbp:is_known_for
|
high performance
high energy density
stability at room temperature
good handling properties
lower cost than liquid hydrogen
|
|
gptkbp:is_part_of
|
RP family of propellants
hypergolic propellant systems
kerolox engines
|
|
gptkbp:is_used_by
|
gptkb:bird
|
|
gptkbp:is_used_in
|
gptkb:Falcon_9
gptkb:Antares_rocket
gptkb:SLS
gptkb:Electron_rocket
gptkb:Space_X_rockets
gptkb:Viking_rockets
gptkb:rocket
gptkb:Atlas_V
|
|
gptkbp:population
|
810 kg/m³
approximately 810 kg/m³
|
|
gptkbp:produced_by
|
refining crude oil
|
|
gptkbp:storage
|
room temperature
|
|
gptkbp:suitable_for
|
RP-2
|
|
gptkbp:used_in
|
gptkb:rocket
|