S265

Slow burning extruded propellant for magnum revolvers

Category: 
Extruded Propellant

Thermochemical Properties

Propellant Flame Temperature Specific Energy Heat of Explosion Ratio of Specific heats Covolume Density
(K) (°C) (°F) (J/g) (J/g) (Cal/g) (Cp/Cv) (cm³/g) (g/cc)
S265 3 062 2 789 5 052 1 030 3 667 876 1.237 1.003 1.55

S265 Lot Velocity Variation Relative to the Reference Lot

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