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Rfna AEROZINE50 — Rocket Propellant Properties
2.20 dimensionless, 279 s, 272 s
rfna aerozine50 rocket propellant properties reference data. This dataset covers 1 row. Key parameters: isp frozen s 272 s; avg specific gravity 1.27 dimensionless; mixture ratio 2.20 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 Frozen S (s) | Isp Shifting S (s) | Metal Content Pct (%) | Mixture Ratio (dimensionless) | Mol Mass Exhaust Kg Mol (kg/mol) | Oxidizer | Propellant Type | Source Method |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Rfna AEROZINE50 | 1.27 | 1,000 | 5,710 | 3,172 | 5,580 | 1,701 | 40 | Aerozine-50 | 1.22 | 272 | 279 | 0 | 2.2 | 22.4 | Rfna | Liquid Bipropellant | Sutton Table 5-5 Rfna / 50% Udmh + 50% N2H4 (Aerozine-50) at MR=2.20. Pc=1000 psia, Pe=14.7 psia, Optimum expansion. Is SHIFTING=279 s, Is FROZEN=272 s. C*=1701 m/s. Tc=3172 K. M=22.4 kg/mol. K=1.22. |
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