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| Specification | |
|---|---|
| Applications | Titan family upper stage |
| Propellants | LOX/RP-1 or storables, ground tested with LOX/LH2 |
| Thrust in Vacuum | 105,000 lb |
| Thrust at Sea Level | ???? |
| Isp in vacuum(s) | 316 |
| Isp at sea level | ???? |
| Mixture Ratio | 1.78:1 |
| Weight | 1314 lb |
| Chamber Pressure | 860 psia |
| Expansion Ratio | 49.2:1 |
| Engine Cycle | ???? |
| Pump Design Pressures | ???? |