Leros 20R (Atlantic Research Corporation)

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

Leros 20R engine
Engine statistics
Specification
Injector Unlike doublets, fuel film cooling
Valve MOOG 51-127 torque motor
Thrust Chamber CVD Rhenium-Iridium
Expansion Cone CVD Rhenium-Iridium
Propellants MON3, MMH
Thrust 5 lbf
Minimum Isp 307 sec
Mixture Ratio 0.8
Area Ratio 180
Inlet Pressure 235 psia
Mass 1.25 lbm
Envelope 9.8" * 2.4"
























Leros 20H : CGT 1