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Lox RP1 Lower Mr — Rocket Propellant Properties
2.24 dimensionless, 300 s, 1,774 m/s
lox rp1 lower mr rocket propellant properties reference data. This dataset covers 1 row. Key parameters: avg specific gravity 1.01 dimensionless; mixture ratio 2.24 dimensionless; gamma exhaust 1.24 dimensionless.
| Propellant Id | Avg Specific Gravity (dimensionless) | 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 | Gamma Exhaust (dimensionless) | Isp Shifting S (s) | Metal Content Pct (%) | Mixture Ratio (dimensionless) | Mol Mass Exhaust Kg Mol (kg/mol) | Oxidizer | Propellant Type | Source Method |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Lox RP1 Lower Mr | 1.01 | 1,000 | 6,428 | 3,571 | 5,820 | 1,774 | 40 | RP1 | 1.24 | 300 | 0 | 2.24 | 21.9 | Lox | Liquid Bipropellant | Sutton Table 5-5 LOX/RP-1 at MR=2.24 (lower Mr row). Pc=1000 psia, Pe=14.7 psia, Optimum expansion. Is SHIFTING=300 s. C*=1774 m/s. Tc=3571 K. M=21.9 kg/mol. |
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