Labels:airplane | bulletin board | flap | lamp | monitor | shutter | sky | space rocket | windowpane OCR: FRONT VIEW TOP VIEW REAR VIEW BOTTOM VIEW PAYLOAD ORBITAL MANEUVERING SYSTEM/ RUDDER/ BAY DOORS REACTION CONTROL SPEED BRAKE SYSTEM MODUL FORWARD REACTION AFT REACTION CONTROL SYSTEM CONTROL MODULE SYSTEM NASA MAIN ENGINES United Statesc BODY FLAP ELEVONS NOSE LANDING GEAR SIDE HATCH MAIN LANDING GEAR DIMENSI IONS AND WE IGHT WING SPAN 23 79 m (78 .06 FT) LENGTH 24 (122 FT HEIGHT 25 (56 58 ET TREAD WIDTH 6.91 (22 67 FT) GROSS TAKEOFF WEIGHT VARIABLE GROSS LANDING WEIGHT VARIABLE INERT WEIGHT (APPROX) 14 844 ka (165 000 L8) MINIMUM GROUND CLEARANCES BODY FLAP (AFT END 3.68 (12.07 FT) MAIN GEAR DOOR 0.87 T (2.85 FT) NOSE GEAR (DOOR 0.90 TY 12 96' FT) WINGTIP 3.63 (11 .92 FT) BUDDER MODULES FLEVONS DIMENSIONS TAKEOFP
