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| Specification | |
|---|---|
| Applications | Delta II,III,IV EELV second stage |
| Propellants | Aerozine 50/N2O4 |
| Thrust in Vacuum | 9753 lb |
| Isp in vacuum(s) | 320.5 s |
| Mixture Ratio | 1.9:1 |
| Weight | 275 lb |
| Chamber Pressure | 130 psia |
| Expansion Ratio | 65:1 |
| Engine Cycle | Pressure Fed |