
The
Mobile
Launcher Platform is a two-story steel structure which provides a
transportable launch base for the Space Shuttle. First used in the
Apollo/Saturn program, the Platforms underwent modifications for the
Shuttle.
The main body of each Platform
is 25 feet (7.6 meters) high, 160 feet (49 meters) long, and 135 feet (41
meters) wide. At their parking sites north of the Vehicle Assembly Building,
in the Vehicle Assembly Building high bays and at the launch pads, the
Mobile Launcher Platforms rest on six pedestals 22 feet (6.7 meters) high.
Unloaded, a Platform weighs
about 8.23 million pounds (3.73 million kilograms). With an unfueled Shuttle
aboard, it weighs about 11 million pounds (5 million kilograms).
The main body of the Platform
provides three openings - two for the exhaust of the solid rocket boosters
and one for the main engines exhaust.
There are two large devices
called Tail Service Masts, one on each side of the main engines exhaust
hole. The masts provide several umbilical connections to the orbiter,
including a liquid-oxygen line through one and a liquid-hydrogen line
through another. These cryogenic propellants feed into the external tank
from the pad tanks via these connections. At launch, the umbilicals pull
away from the orbiter and retract into the Masts, where protective hoods
rotate closed to shield them from the exhaust flames. Each Tail Service Mast
assembly is 15 feet (4.6 meters) long, 9 feet (2.7 meters) wide, and rises
31 feet (9.4 meters) above the Platform deck.
Other umbilicals carry helium
and nitrogen, as well as ground electrical power and communications links.
Eight attach posts, four on the
aft skirt of each SRB, support and hold the Space Shuttle on the Mobile
Launcher Platform. These posts fit on counterpart posts located in the
Platform's two solid rocket booster support wells. The space vehicle
disconnects from the Platform by explosive nuts which release the giant
studs linking the solid rocket attach posts with the Platform support posts.
Each Mobile Launcher Platform
has two inner levels containing electrical, test and propellant-loading
equipment.
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