Back to the Purdue AAE Propulsion main page.
Back to the Satellite Propulsion page.
| 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" |