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T-09
minutes
-- the Ground Launch Sequencer (GLS)
is activated and the terminal countdown
begins. All
countdown functions are now automatically
controlled by the GLS computer located
in the Firing Room Integration Console.
T-07
minutes, 30 seconds and counting
-- the Orbiter
Access Arm is retracted. Should
an emergency occur requiring crew evacuation
from the Orbiter, the arm can be extended
either manually or automatically in
about 15 seconds.
T-05
minutes, 00 seconds and counting
-- the crew activates the Auxiliary
Power Units (APU) to provide pressure
to the Shuttle's three hydraulic systems
which move the main engine nozzles and
the aero-surfaces.
T-04
minutes, 55 seconds and counting
-- the liquid oxygen vent on the external
tank is closed.
T-04
minutes, 00 seconds and counting
-- the final helium purge of the Shuttle's
three main engines is initiated in preparation
for engine start.
T-02
minutes, 50 seconds and counting
-- the external tank Gaseous
Oxygen Vent Hood -- known as the
beanie cap -- is raised and retracted.
It had been in place during tanking
operations to prevent ice buildup on
the oxygen vents.
T-02
minutes, 00 seconds and counting
-- STS-107 flight crew -- close and
lock helmet visors.
T-01
minutes, 57 seconds and counting
-- the external tank's liquid hydrogen
is brought to flight pressure by closing
the boil off vent, as was done earlier
with the liquid oxygen vent.
T-00
minutes, 50 seconds and counting
-- Orbiter transfers from ground to
internal power.
T-00
minutes, 31 seconds and counting
-- the Shuttle's onboard computers start
their terminal launch sequence.
T-00
minutes, 16 seconds and counting
-- the Sound
Suppression System is activated
and 400,000
gallons of water begins to pour
onto the deck of the Mobile
Launch Platform and Pad B to protect
the Shuttle from acoustical damage at
liftoff.
T-00
minutes, 10 seconds and counting
-- the "go for main engine start"
command is issued by the Ground Launch
Sequencer. (The GLS retains the capability
to command main engine stop until just
before the Solid Rocket Boosters are
ignited.) Concurrently, flares are ignited
under the main engines to burn away
any residual gaseous hydrogen that may
have collected in the vicinity of the
main engine nozzles. A half second later,
the flight computers order the opening
of valves which allow the liquid hydrogen
and oxygen to flow into the engine's
turbo pumps.
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