|
gptkbp:instanceOf
|
rocket propellant
|
|
gptkbp:alternativeTo
|
hydrazine
liquid hydrogen
|
|
gptkbp:aroma
|
mild
|
|
gptkbp:boilingPoint
|
150–275°C
|
|
gptkbp:color
|
clear
|
|
gptkbp:density
|
0.81 g/cm³
|
|
gptkbp:developedBy
|
gptkb:Rocketdyne
|
|
gptkbp:flammability
|
high
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
RP-1 kerosene
|
|
gptkbp:introduced
|
1950s
|
|
gptkbp:lessEfficientThan
|
liquid hydrogen
|
|
gptkbp:meltingPoint
|
-60°C
|
|
gptkbp:powerSource
|
43 MJ/kg
|
|
gptkbp:regulates
|
gptkb:ASTM_D1655
|
|
gptkbp:relatedTo
|
gptkb:Jet-A_kerosene
RP-2 kerosene
|
|
gptkbp:saferThan
|
hydrazine
|
|
gptkbp:storage
|
ambient temperature
|
|
gptkbp:toxicity
|
low
|
|
gptkbp:type
|
refined petroleum
|
|
gptkbp:usedBy
|
gptkb:satellite
gptkb:Antares_rocket
gptkb:Angara_rocket
gptkb:Soyuz_rocket
gptkb:Saturn_I
gptkb:Saturn_IB
gptkb:Saturn_V
gptkb:Falcon_9
gptkb:Delta_II
gptkb:Electron_rocket
|
|
gptkbp:usedFor
|
liquid oxygen
booster engines
first stage propulsion
|
|
gptkbp:usedIn
|
gptkb:R-7_Semyorka
gptkb:Thor_rocket
gptkb:Vulcan_rocket
gptkb:Ariane_1
gptkb:Ariane_2
gptkb:Ariane_3
gptkb:Firefly_Alpha
gptkb:Long_March_11
gptkb:Long_March_6
gptkb:Long_March_7
gptkb:Long_March_8
liquid-fueled rockets
Hyperbola-1
Hyperbola-2
N-1 rocket
Titan I rocket
|
|
gptkbp:bfsParent
|
gptkb:SM-68_Titan_I
gptkb:Convair_SM-65_Atlas
|
|
gptkbp:bfsLayer
|
7
|