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Line 29: \|thrust = \|thrust_at_altitude= \|thrust(Vac) ={{convert\|~~788~~882\|kN\|lbf\|abbr=on}} \|thrust(SL) ={{convert\|~~882~~788\|kN\|lbf\|abbr=on}} \|throttle_range = \|thrust_to_weight=

RD-250: Difference between revisions