Apollo H-1 (Rocketdyne)
| Specification | |
|---|---|
| Applications | Saturn 1B first stage (8 clustered) |
| Propellants | LOX/RP-1 |
| Thrust at Sea Level | 205,000 lb |
| Isp at sea level | 263 s |
| Mixture Ratio | 2.23:1 |
| Weight | 2009 lb |
| Chamber Pressure | 700 psia |
| Area Ratio | 8:1 |
| Engine Cycle | |
| Pump Design Pressures |
J2 : Satellite Systems 