Leros 20 (Atlantic Research Corporation)

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

Leros 20 engine
Engine statistics
Specification
Injector Unlike doublets, fuel film cooling
Valve MOOG 51-127 redundant torque motor
Thrust Chamber C103/R512E
Expansion Cone C103/R512E
Propellants MON3, MMH
Thrust 5 lbf
Minimum Isp 293 sec
Minimum I bit 0.006 lbf-sec
Mixture Ratio 1.65
Area Ratio 180
Inlet Pressure 220 psia
Mass 1.25 lbm
Envelope 8.7" * 2.4"


























Leros 2R : Leros 20H