Liquid engine calculator

Input

Select a propellant combination:
Combustion temperature:		Kelvin
Specific Heat Ratio:		[-]
Molar Mass:		gram/mol
Chamber pressure:		[bar]
Exit pressure:		[bar]
Ambiant pressure:		[bar]
Mass flow:		[kg/s]
Mach inlet:		[-]
Percentage length 15 degree cone:		[%]
Inlet angle:		[degrees]
Bell angle throat:		[degrees]
Bell angle exit:		[degrees]
L*:		[m]
Correction factor c*:		[-]
Correction factor cf:		[-]

Result