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LEROS-1B
Liquid propellant apogee engine manufactured by Moog.

Thrust: 635 N (142 lbf). Specific impulse: 318 s.

Subtopics
LEROS-1C Liquid propellant apogee engine manufactured by Moog.
LEROS-2B Liquid propellant apogee engine manufactured by Moog.
LEROS-4 High thrust liquid propellant apogee engine developed by Moog for the European Space Agency’s (ESA) Mars Robotic Exploration Program.
Country: UK. Propellants: MON/N2H4. Agency: Moog.
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