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| Specification | Two chambers |
|---|---|
| Applications | Titan launch vehicle family |
| Propellants | LOX/RP-1 or storables, ground tested with LOX/LH2 |
| Thrust in Vacuum | 276,300 x 2 = 552,600 lb |
| Thrust at Sea Level | ???? |
| Isp in vacuum(s) | 304 |
| Isp at sea level | ???? |
| Mixture Ratio | 1.91:1 |
| Weight | 4780 lb |
| Chamber Pressure | 860 psia |
| Expansion Ratio | 16.7:1 |
| Engine Cycle | ???? |
| Pump Design Pressures | ???? |