Launch-3 Days (Tuesday, April 26)
Prepare for the start of the STS-134 launch countdown
Perform the call to stations (1:30 p.m.)
Countdown begins at the T-43 hour mark (2 p.m.)
Begin final vehicle and facility closeouts for launch
Check out backup flight systems
Launch-2 Days (Wednesday, April 27)
Configure avionics systems for launch
Review flight software stored in mass memory units and display systems
Verify backup flight system software in Endeavour's general purpose computer
Activate and test navigational systems (1 a.m.)
Complete preparations to load power reactant storage and distribution system (5 a.m.)
Flight Crew Equipment early stow and flight deck preliminary inspections complete (6 a.m.)
Enter 4-hour built-in hold at T-27 hours (6 a.m.)
Clear launch pad of all nonessential personnel
Perform test of the vehicle's pyrotechnic initiator controllers and range safety system
Resume countdown (10 a.m.)
Begin operations to load cryogenic reactants into Endeavour's fuel cell storage tanks (10 a.m.)
Enter 8-hour built-in hold at T-19 hours (6 p.m.)
Demate orbiter mid-body umbilical unit (10:30 p.m.)
Resume orbiter and ground support equipment closeouts
Launch-1 Day (Thursday, April 28)
Resume countdown (2 a.m.)
Main engine avionics, pneumatics and controller checkout (2 a.m.)
External Tank feedline inspection/camera cleaning
Flight Crew Equipment stowage
Begin removal of pad ground support equipment
Enter built-in 13 hours, 22 minute hold at T-11 hours (10 a.m.)
Activate the orbiter's communications systems
Lower engine support platforms, retract access platforms
External Tank Inspections
Complete Flight Crew Systems time critical stowage (middeck payloads)
Rotating Service Structure begins move away from Endeavour to the park position (7 p.m.)
Perform ascent switch list
Fuel cell flow-through purge complete
Resume countdown at T-11 hours (11:22 p.m.)
Launch Day (Friday, April 29)
Activate the orbiter's fuel cells (12:32 a.m.)
Clear the blast danger area of all nonessential personnel
Switch Endeavour's purge air to gaseous nitrogen (1:22 a.m.)
Complete final walkdowns
Enter 2-hour built-in hold at the T-6 hour mark (4:22 a.m.)
Complete tanking preparations
Launch team verifies no violations of launch commit criteria prior to cryogenic loading of the external tank
Clear pad of all personnel
Resume countdown (6:22 a.m.)
Chill down propellant transfer lines (6:22 a.m.)
Begin loading the external fuel tank with about 500,000 gallons of cryogenic propellants (about 6:32 a.m.)
Enter 2-hour, 30-minute built-in hold at T-3 hours (9:22 a.m.)
Perform inertial measurement unit preflight calibration
Align Merritt Island Launch Area tracking antennas
Complete filling the external tank with its flight load of liquid hydrogen and liquid oxygen propellants (about 9:22 a.m.)
Final Inspection Team and Closeout Crew proceeds to launch pad
Resume countdown at T-3 hours (11:52 a.m.)
Perform open loop test with Eastern Range
Crew departs Operations and Checkout Building for the pad (11:58 a.m.)
Complete closeout preparations in the White Room
Check cockpit switch configurations
Begin Eastern Range final network open loop command checks
Flight crew begins entry into the orbiter (12:28 p.m.)
Astronauts perform air-to-ground voice checks with Launch and Mission Control
Begin to close Endeavour's crew hatch (1:32 p.m.)
Perform hatch seal and cabin leak checks
Complete White Room closeout
Closeout crew moves to fallback area
Primary ascent guidance data is transferred to the backup flight system
Enter 10-minute hold at T-20 minutes (2:32 p.m.)
NASA test director conducts final launch team briefings
Resume countdown at T-20 minutes (2:42 p.m.)
Transition the orbiter's onboard computers to launch configuration
Start fuel cell thermal conditioning
Close orbiter cabin vent valves
Transition backup flight system to launch configuration
Enter estimated 45-minute hold at T-9 minutes (2:53 p.m.)
Final launch window determination
Launch director, Mission Management Team and NASA test director conduct final polls for "go/no go" to launch
Resume countdown at T-9 minutes (about 3:38 p.m.)
Start automatic ground launch sequencer (T-9 minutes)
Retract orbiter crew access arm (T-7:30)
Start APU recorders (T-6:15)
Start auxiliary power units (T-5)
Terminate liquid oxygen replenish (T-4:55)
Start orbiter aerosurface profile test (T-3:55)
Start main engine gimbal profile test (T-3:30)
Pressurize liquid oxygen tank (T-2:55)
Begin retracting the gaseous oxygen vent arm (T-2:50)
Fuel cells to internal reactants (T-2:35)
Pressurize liquid hydrogen tank (T-1:57)
Deactivate bi-pod heaters (T-1:52)
Deactivate solid rocket booster joint heaters (T-0:50 seconds)
Orbiter transfers from ground to internal power (T-0:50 seconds)
Ground launch sequencer go for auto sequence start (T-0:31 seconds)
Booster gimbal profile (T-0:21 seconds)
Ignition of three space shuttle main engines (T-6.6 seconds)
Booster ignition and liftoff (T-0)
Preferred launch time: 3:47 p.m.
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