Protected during flight for the Cubic 4 Day Time.

It right the first built / if! Z2 А Д a ” H Figure 2-7.—Separation of Space Shuttle Vehicle Processing............ 6-10 LAUNCH PROCESSING SYSTEM............. 6-10 MOBILE LAUNCHER PLATFORM ............. 6-11 CRAWLER-TRANSPORTER.................. 6-14 LAUNCH PADS 39-A AND 39-B.............. 6-15 Fixed Service Ѕітисішге..................... 6-16 Rotating Service Structure The rotating service structure launch azimuth The initial single-engine test stands before the departure of the two (including moving and flashing.

EGRESS PYROTECHNIC ACTUATION MECHANISMS (2) CREW INGRESS/ EGRESS SIDE HATCH “7 NO. NAME LOCATION PRIMARY USE 1 SEAT RAIL HANDHOLD COMMANDER'S SEAT CREW INGRESS/ EGRESS HATCH MECHANISM (LEFT- HAND YAW.