LEROS-4 (original) (raw)

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LEROS-4

Part of LEROS-1B

High thrust liquid propellant apogee engine developed by Moog for the European Space Agency�s (ESA) Mars Robotic Exploration Program.

Thrust: 1.10 kN (247 lbf). Specific impulse: 325 s.

Country: UK. Propellants: MON/N2H4. Agency: Moog.

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