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Rocket Propellant Properties: lox ch4
Rocket propellant performance data — specific impulse, characteristic velocity, chamber conditions for bipropellant, solid, and monopropellant combinations
| propellant id | chamber pressure psia (psia) | chamber temp deg r (deg R) | chamber temp k (K) | cstar ft s (ft/s) | cstar m s (m/s) | expansion ratio (dimensionless) | fuel | isp vac s (s) | mixture ratio (dimensionless) | oxidizer | source method |
|---|---|---|---|---|---|---|---|---|---|---|---|
| lox ch4 | 300 | 6,300 | 3,500 | 6,100 | 1,859.28 | 40 | CH4 | 370 | 3.4 | LOX | Fallback seed (RocketCEA package unavailable) |
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