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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-110 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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