LEROS-1B (original) (raw)
Thrust: 635 N (142 lbf). Specific impulse: 318 s.
LEROS-4 High thrust liquid propellant apogee engine developed by Moog for the European Space Agency�s (ESA) Mars Robotic Exploration Program.
Thrust: 635 N (142 lbf). Specific impulse: 318 s.
LEROS-4 High thrust liquid propellant apogee engine developed by Moog for the European Space Agency�s (ESA) Mars Robotic Exploration Program.