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| Specification | |
|---|---|
| Applications | Second Stage of Delta, SDI ground tests |
| Propellants | N2O4 and UDMH/N2H4 |
| Thrust in Vacuum | 9800 lb |
| Isp in vacuum(s) | 303 |
| Mixture Ratio | 1.60:1 |
| Weight | 300 lb |
| Chamber Pressure | 104 psia |
| Expansion Ratio | ???? |
| Engine Cycle | ???? |
| Pump Design Pressures | ???? |