Variable Thrust Engine (TRW)
Specification | |
---|---|
Applications | Lunar Descent Module, Delta second stage |
Propellants | N2O4 and MMH |
Thrust | 130 to 1300? lbf |
Isp in vacuum(s) | |
Mixture Ratio | 1.64 |
Weight | 15 lbm |
Chamber Pressure | 100-11??? psia |
Area Ratio | 125:1 |
Engine Cycle | ??? |
Pump Design Pressures | ??? |