Leros 2R (Atlantic Research Corporation)

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

Leros 2r engine
Engine statistics
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"
























Leros 2 : Leros 20