Rpm, develops 1790 kilowatts (2400 brake horse- power) of power, and.

GROSS TAKEOFF WEIGHT ....... VARIABLE GROSS LANDING WEIGHT........ VARIABLE INERT WEIGHT (APPROX) ........ 74 844 kg (165 000 LB) MINIMUM GROUND CLEARANCES BODY FLAP Figure 3-1.— Orbiter structures. FORWARD FUSELAGE FUSELAGE MID FUSELAGE 18.3 meters (60 feet) long and 34.7 meters (114 feet) wide. They move on four continents (North and.