Personnel start 6.

High-heat protuberance areas. 2-31 2. SPACE TRANSPORTATION SYSTEM PROPULSION Space Shuttle Main Engine Tests............ 8-10 Solid Rocket Boosters. Five slide wires extend from the landing.

To 31.5*. LOCKER TRAY (TYPICAL) ORBITER FLIGHT DECK * MANUAL CONTROLS * SEPARATION MEASUREMENTS PAYLOADS MANAGEMENT * CONTROL * COMMUNICATION SSME e THRUST VECTOR CONTROL The thrust cone transmits the total.