Specification | |
---|---|
Applications | Atlas IIAR |
Propellants | LOX/kerosene |
Thrust in Vacuum | 933,000 lb |
Thrust at Sea Level | 860,400 |
Isp in vacuum(s) | ???? |
Isp at sea level | 311 sec |
Mixture Ratio | 2.6:1 |
Weight | 11675 lb |
Chamber Pressure | 3734 psia |
Area Ratio | 36.4:1 |
Engine Cycle | ???? |
Pump Design Pressures | ???? |