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Flight
crew departs the
Operations and Checkout Building (O&C) and proceeds to
the Launch Pad (live on NASA
TV).
Astronauts arrive
at the
launch pad and begin entering the orbiter.
Close-out Crew begins
sealing off Atlantis' crew compartment.
At approximately
T-50 minutes and counting, Pilot Stephen Frick configures
switches in the cockpit to pre-activate the orbiter's three water
spray boilers. Each of the orbiter's three hydraulic systems
has a boiler used to cool the system's hydraulic fluid and Auxiliary
Power Unit lubrication oil. Boiler steam is vented overboard.
During the launch,
orbital checkout, and reentry through landing phases, the spray
boilers are activated if the hydraulic fluid exceeds 208
degrees Fahrenheit or 250
degrees Fahrenheit for the lubrication oil. The spray boilers
are located in the orbiter's aft fuselage and hold about 120
pounds of water.
At T-45
minutes and counting, the Terminal Count Range safety closed-loop
test begins. This test verifies the paths the destruct signal
would travel and confirms that the Shuttle’s range safety receiver
responds correctly to the commands sent. This is also a health
check of the range safety signal. Console operators in the Eastern
Test Range Control Center at Cape Canaveral Air Station will also
get verification that the orbiter has received the signal.
This test normally takes about five minutes to complete and is
done to ensure down range shipping lanes and the booster splashdown
area are clear and that the tracking station is ready.
Also at this
time, NASA Test Director, Steve Altemus, coordinates with Mission
Control in Houston, Texas, to switch Atlantis' S-band antennas
to high power mode and to configure the onboard communications
system so that it will transmit and receive by radio at liftoff
(during launch countdown, communications
with the orbiter are hard wired). This system can communicate
either directly between the orbiter and ground or through the
TDRS satellite system.
By T-40
minutes and counting, the Ground Launch Sequencer mainline
computer program is active and begins processing data. This program
will monitor various key commands and systems prior to assuming
control of the countdown at the T-9 minute and counting mark.
By T-30 minutes,
the Orbital Maneuvering System (OMS) gaseous nitrogen tanks have
been pressurized for launch. Gaseous nitrogen is used to operate
the valves allowing the hypergolic propellants to flow into the
OMS engines during flight.
At about this same
time in the countdown, the post launch inspection and safing teams
begin assembling approximately one mile from the launch pad.
Within
the next minute or so, the preflight test of Atlantis' Master
Events Controller (MEC) is completed. The MEC relays commands
from the orbiter's computers to fire explosive charges to the
Solid Rocket Booster hold-down bolts at launch and to separate
the tank and twin boosters in flight.
By the T-25 minute
mark, the Closeout Crew has evacuated the launch pad.
Over the next few
minutes, Commander Michael Bloomfield performs a series of voice
checks, configures Return-To-Launch-Site (RTLS) altimeter settings,
and completes other preflight checklist items.
Also during this
period, the Kennedy Space Center Launch and Johnson Space Center
Flight Directors are briefed about impending launch and RTLS weather
conditions.
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