Shuttle Mission STS-108
Orbiter - Endeavour
December 4, 2001

"T" stands for scheduled liftoff time, "-" stands for minus, "H" stands for hours, "M" stands for minutes and
"S" stands for seconds.

T-09M00S & Counting.....


 

Primary Event Description

Date
Eastern Standard Time

Resume countdown from scheduled hold period.

 December 4, 2001
5:36 P.M.

 

STS-108 Mission Patch

Other events occurring during this time frame:

 
è

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.

è 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.
è T-05 minutes, 15 seconds and counting -- the Master Control Console (MCC) transmits a command that activates the orbiter's operational instrumentation recorders. These recorders store information relating to ascent, on-orbit and descent performance during the mission.  These data are analyzed after landing.
è 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.
è T-04 minutes, 55 seconds and counting -- the liquid oxygen vent on the external tank is closed. It had been open to allow the super-cold liquid oxygen to boil off, thus preventing over pressurization while the tank remained near its full level.  Now, with the vent closed, preparations are made to bring the tank to its flight pressure. This occurs at T minus 2 minutes, 55 seconds.
è 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.  
è T-03 minutes, 55 seconds and counting -- the orbiter's elevons, speed brakes and rudder are moved through a pre-programmed series of maneuvers to position them for launch. This is known as the aero-surface profile.
è T-03 minutes, 30 seconds and counting -- the ground power transition occurs and the Shuttle's fuel cells transition to internal power. Up to this point, ground power had augmented the fuel cells.
è 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.
è T-02 minutes, 00 seconds and counting -- STS-108 flight crew -- close and lock helmet visors.
è 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. However, during the hydrogen boil off of, the gas is piped out to an area adjacent to the launch pad where it is burned off.
è T-00 minutes, 50 seconds and counting -- Orbiter transfers from ground to internal power.
è T-00 minutes, 31 seconds and counting -- the Shuttle's on-board computers start their terminal launch sequence. Any problem after this point will require calling a "hold" and the countdown recycled to T minus 20 minutes. Meanwhile, the Ground Launch Sequencer (GLS) continues to monitor several hundred launch commit functions and is able automatically to call a "hold" or "cutoff" if a problem occurs.
è 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.
è 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.