Leros 20 (Atlantic Research Corporation)
![Leros 20 engine](../../../images/rockets/satellites/leros20.gif)
Specification | |
---|---|
Injector | Unlike doublets, fuel film cooling |
Valve | MOOG 51-127 redundant torque motor |
Thrust Chamber | C103/R512E |
Expansion Cone | C103/R512E |
Propellants | MON3, MMH | Thrust | 5 lbf |
Minimum Isp | 293 sec |
Minimum I bit | 0.006 lbf-sec |
Mixture Ratio | 1.65 |
Area Ratio | 180 |
Inlet Pressure | 220 psia |
Mass | 1.25 lbm |
Envelope | 8.7" * 2.4" |
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