Leros 20H (Atlantic Research Corporation)

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

Leros 20H engine
Engine statistics
Specification
Injector Unlike doublets, fuel film cooling
Valve MOOG 51-131 torque motor
Thrust Chamber C103/R512E
Expansion Cone C103/R512E
Propellants MON3, Hydrazine
Thrust 5 lbf
Minimum Isp 300 sec
Mixture Ratio 0.8
Area Ratio 180
Inlet Pressure 235 psia
Mass 0.9 lbm
Envelope 7.7" * 2.4"























Leros 20 : Leros 20R