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| T- 34 Hours | Booster is prepared for fuel loading |
| T- 6:00:00 | Batteries are installed in booster |
| T- 5:30:00 | State commission gives go to take launch vehicle |
| T- 5:15:00 | Crew arrives at site 254 |
| T- 5:00:00 | Tanking begins |
| T- 4:20:00 | Spacesuit donning |
| T- 4:00:00 | Booster is loaded with liquid oxygen |
| T- 3:40:00 | Crew meets delegations |
| T- 3:10:00 | Reports to the State commission |
| T- 3:05:00 | Transfer to the launch pad |
| T- 3:00:00 | Vehicle first and second stage oxidizer fueling complete |
| T- 2:35:00 | Crew arrives at launch vehicle |
| T- 2:30:00 | Crew ingress through orbital module side hatch |
| T- 2:00:00 | Crew in re-entry vehicle |
| T- 1:45:00 | Re-entry vehicle hardware tested Suits are ventilated |
| T- 1:30:00 | Launch command monitoring and supply unit prepared Orbital compartment hatch tested for sealing |
| T- 1:00:00 | Launch vehicle control system prepared for use; gyro instruments activated |
| T - :45:00 | Launch pad service structure halves are lowered |
| T- :40:00 | Re-entry vehicle hardware testing complete; leak checks performed on suits |
| T- :30:00 | Emergency escape system armed; launch command supply unit activated |
| T- :25:00 | Service towers withdrawn |
| T- :15:00 | Suit leak tests complete; crew engages personal escape hardware auto mode |
| T- :10:00 | Launch gyro instruments uncaged; crew activates on-board recorders |
| T- 7:00 | All prelaunch operations are complete |
| T- 6:15 | Key to launch command given at the launch site Automatic program of final launch operations is activated |
| T- 6:00 | All launch complex and vehicle systems ready for launch |
| T- 5:00 | Onboard systems switched to onboard control Ground measurement system activated by RUN 1 command Commander's controls activated Crew switches to suit air by closing helmets Launch key inserted in launch bunker |
| T- 3:15 | Combustion chambers of side and central engine pods purged with nitrogen |
| T- 2:30 | Booster propellant tank pressurization starts Onboard measurement system activated by RUN 2 command Prelaunch pressurization of all tanks with nitrogen begins |
| T- 2:15 | Oxidizer and fuel drain and safety valves of launch vehicle are closed Ground filling of oxidizer and nitrogen to the launch vehicle is terminated |
| T- 1:00 | Vehicle on internal power Automatic sequencer on First umbilical tower separates from booster |
| T- :40 | Ground power supply umbilical to third stage is disconnected |
| T- :20 | Launch command given at the launch position Central and side pod engines are turned on |
| T- :15 | Second umbilical tower separates from booster |
| T- :10 | Engine turbopumps at flight speed |
| T- :05 | First stage engines at maximum thrust |
| T- :00 | Fueling tower separates Lift off |