Leros 2R (Atlantic Research Corporation)
![Leros 2r engine](../../../images/rockets/satellites/leros2r.gif)
Specification | |
---|---|
Injector | Unlike doublets, fuel film cooling |
Valve | MOOG 53-180 solenoids |
Thrust Chamber | CVD Rhenium-Iridium |
Expansion Cone | C103/R512E |
Propellants | MON3, MMH | Thrust | 125 lbf |
Minimum Isp | 316 sec |
Mixture Ratio | 1.65 |
Area Ratio | 150 |
Inlet Pressure | 235 psia |
Mass | 8.3 lbm |
Envelope | 28" * 11.4" |
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