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BRAKE/ANTISKID VALVES Figure 4-4.— Orbiter hydraulic system. 4-14 MAIN LANDING GEAR AND NOSE LANDING GEAR VALVES FOUR-CHANNEL SERVOACTUATORS BODY-FLAP ROTARY ACTUATORS RUDDER/ SPEED BRAKE POWER DRIVE UNIT THRUST VECTOR CONTROL The thrust vector control system. Forward Assembly The Solid Rocket Boosters. Each booster is attached to the launch platform. The mid-deck work/dining table is also used during routine flyaround inspections of the human.