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Rocket Propellant Properties: n2o4 mmh
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 |
|---|---|---|---|---|---|---|---|---|---|---|---|
| n2o4 mmh | 300 | 5,800 | 3,222.2222 | 5,600 | 1,706.88 | 40 | MMH | 330 | 2.1 | N2O4 | Fallback seed (RocketCEA package unavailable) |
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