Artemis
Run Simulation
Guns
Shells
Chambering
Propellants
Grains
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Name
*
Country of Origin
---------
Austria-Hungary
France
Germany
Italy
Japan
Russia/USSR
United States
United Kingdom
other
not set
Specific Heat Ratio
*
dimensionless
Specific Force
*
kJ/kg
cal/lb
cal/g
ft·lbf/lb
in·lbf/lb
Flame Temperature
*
°K
°R
°C
°F
Co-volume
*
mm³/kg
in³/lb
mm³/g
cm³/g
m³/kg
Density
*
kg/mm³
g/cm³
lb/in³
kg/m³
Burn Rate Coefficient
*
m·s⁻¹·MPa⁻¹
in·s⁻¹·psi⁻¹
in·s⁻¹·kpsi⁻¹
mm·s⁻¹·Pa⁻¹
m·s⁻¹·Pa⁻¹
Burn Rate Exponent
*
dimensionless
Comment
Burn rate coefficient and exponent likely need adjusting for specific formulation if not used only as an igniter