MRE-5 Monopropellant Thruster (TRW)

For more than 25 years, TRW monopropellant thrusters have provided continuous on-orbit delta velocity and attitude control service for a variety of spacecraft. All thrusters share the unique TRW head design, utilize Shell 405 catalyst, and incorporate bed loadings consistent with long life.

MRE-5 Monopropellant Thruster

Engine statistics
Specification  
Thrust at max. operating pressure 36 N at 400 psia
Thrust at 275 psia inlet pressure 28 N (6.3 lbf)
Steady State Specific Impulse/th> 232 sec
Minimum impulse-bit at 275 psia 0.11 lbs-sec
Envelope (width * length) 145 mm * 264 mm
Weight (single thruster module) NA
Weight (dual thruster module) 1.5 kg (3.2 lbm)
Maximum throughput 456 kg
Maximum cycles 28,512
Operating Pressure Range 70-475 psia
Thruster Valve Power at 28 Vdc 30 W





















MRE-4 : MRE-15