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| Specification | |||
|---|---|---|---|
| Applications | Soviet N-1 moon rocket (1970), Kistler K-1 RLV (present) | ||
| Propellants | LO2/HC | ||
| Thrust in Vacuum | 339,000 lbf | ||
| Thrust at Sea Level | |||
| Isp in vacuum(s) | 331 | ||
| Isp at sea level | 297 | ||
| Mixture Ratio | 2.6:1 | ||
| Weight | 2725 lb | ||
| Chamber Pressure | 2109 psia | ||
| Expansion Ratio | ???? | ||
| Engine Cycle | ???? | ||
| Pump Design Pressures | ???? |