Specification | |
---|---|
Injector | Unlike doublets, fuel film cooling |
Valve | MOOG 53-180 solenoids |
Thrust Chamber | C103/R512E |
Expansion Cone | C103/R512E |
Propellants | MON3, MMH |
Thrust | 125 lbf |
Minimum Isp | 312 sec |
Mixture Ratio | 1.65 |
Area Ratio | 150 |
Inlet Pressure | 235 psia |
Mass | 7.5 lbm |
Envelope | 24.9" * 11.4" |