He expected to lower the Orbiter crew module and 1318 kilograms (2905 pounds) of.

LONGERON ELECTRICAL WIRE TRAY PAYLOAD DOOR HINGE STABILIZER (3) SILL LONGERON ЖС. ҒОВУУАНО BOTTOM SKINS Figure 3-10.— Mid fuselage. BULKHEAD FRAME (TITANIUM WEB) GRAPHITE/EPOXY “J” MEMBER FORWARD UPPER CAP ALUMINUM CENTERLINE BEAM ALUMINUM REACTION CONTROL SYSTEM 2 FUEL TANK FORWARD Figure 4-5.— Orbiter auxiliary power Systems. Propellant quantity indicator.—The propellant quantity.