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HYDROCARBON

JP-1

C₁₂H₂₆ (approximate kerosene blend)
FuelStorable at ambient temperatureLow (similar to kerosene)
C₁₂H₂₆ (approximate kerosene blend)
FORMULA
CHEMICAL
260–320 s (with LOX)
SECONDS
ISP RANGE
0.80 g/cm³
KG/M³
DENSITY
175–260°C
°C
BOILING POINT
~170 g/mol
G/MOL
MOLECULAR WEIGHT
Low (similar to kerosene)
RATING
TOXICITY

JP-1 (C₁₂H₂₆ (approximate kerosene blend)) is a hydrocarbon propellant used as a fuel. Storable at ambient temperature. Typical ISP: 260–320 s (with LOX) seconds.

JP-1 was an early jet fuel specification used in some rocket applications, essentially a kerosene with tighter specifications than standard aviation fuel. It was superseded by JP-4, JP-5, and eventually RP-1 for rocket use. JP-1 had a relatively high freezing point which limited its utility in aviation but was acceptable for ground-launched rocket applications.

FormulaC₁₂H₂₆ (approximate kerosene blend)
🔬TypeHydrocarbon
🔥RoleFuel
Density0.80 g/cm³ kg/m³
Molecular Weight~170 g/mol g/mol
🌡Boiling Point175–260°C°C
Melting Point-60°C (freeze point)°C
🎨Color / AppearanceClear to pale straw
📦StorabilityStorable at ambient temperature
CryogenicNo

An early military specification fuel introduced in the late 1940s. Quickly superseded by other JP specifications and RP-1 for rocket applications.

Storable, safe handling, widely available kerosene base

Higher freezing point, less refined than RP-1, variable composition

🚀ISP Range260–320 s (with LOX) seconds
ToxicityLow (similar to kerosene)
CryogenicNo
LOX (Liquid Oxygen)
Early US ballistic missiles

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