Bruce Buckingham
June 4, 2002 SHUTTLE MISSION STS-111 LAUNCH TIME ANNOUNCED FOR LAUNCH ON JUNE 5 REMAINING COUNTDOWN MILESTONES *all times are Eastern Launch-1 Day (Tuesday, June 4) (As of 5 p.m., the countdown clock is in a scheduled built-in hold at the T-11 hour mark) Flight crew equipment late stow Move Rotating Service Structure (RSS) to the park position (about 8:17 p.m.) Perform ascent switch list Fuel cell flow-through purge complete Launch Day (Wednesday, June 5) Resume countdown at T-11 hours (2:27 a.m.) Activate the orbiter's fuel cells (3:37 a.m.) Clear the blast danger area of all non-essential personnel Switch Endeavour's purge air to gaseous nitrogen (4:42 a.m.) Enter planned 1-hour built-in hold at the T-6 hour mark (7:27 a.m.) Launch team verifies no violations of launch commit criteria prior to cryogenic loading of the external tank Clear pad of all personnel Pre-chilldown of propellant transfer lines Begin loading the external tank with about 500,000 gallons of cryogenic propellants (about 7:57 a.m.) Resume countdown at T-6 hours (8:27 a.m.) Complete filling the external tank with its flight load of liquid hydrogen and liquid oxygen propellants (about 10:57 a.m.) Enter planned 2-hour built-in hold at T-3 hours (11:27 a.m.) Final Inspection Team proceed to launch pad Perform inertial measurement unit preflight calibration Align Merritt Island Launch Area (MILA) tracking antennas Perform open loop test with Eastern Range Resume countdown at T-3 hours (1:27 p.m.) Complete close-out preparations in the white room Check cockpit switch configurations Begin Eastern Range final network open loop command checks Primary ascent guidance data is transferred to the backup flight system Enter planned 10-minute hold at T-20 minutes (4:07 p.m.) NASA Test Director conducts final launch team briefings Complete inertial measurement unit preflight alignments Resume countdown at T-20 minutes (4:17 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 (4:28 p.m.) 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 5:14 p.m.) Start automatic ground launch sequencer (T-9:00 minutes) Retract orbiter crew access arm (T-7:30) Start mission recorders (T-6:15) Start Auxiliary Power Units (T-5:00) Arm SRB and ET range safety safe and arm devices (T-5:00) Start liquid oxygen drainback (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 retraction of the gaseous oxygen vent arm (T-2:55) Fuel cells to internal reactants (T-2:35) Pressurize liquid hydrogen tank (T-1:57) Deactivate SRB joint heaters (T-1:00) Orbiter transfers from ground to internal power (T-0:50 seconds) Ground Launch Sequencer go for auto sequence start (T-0:31 seconds) SRB gimbal profile (T-0:21 seconds) Ignition of three Space Shuttle main engines (T-6.6 seconds) SRB ignition and liftoff (T-0) -- end -- The Kennedy Space Center (KSC) Newsroom offers an electronic subscription service for status reports and news releases issued from KSC. There are two possible ways to subscribe. You may send a blank e-mail message to ksc-news_release-subscribe@kscnews.ksc.nasa.gov or follow the instruction on the Web site at http://kscnews.ksc.nasa.gov. The system will confirm the request via e-mail. |