Leros 2 (Atlantic Research Corporation)

Recently Royal Ordnance. a division of British Aerospace, sold their liquid rocket engines division to Atlantic Research Corporation.

Leros 2 engine
Engine statistics
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"
























Leros 1R : Leros 2R