LAUNCH DAY
PRE-LAUNCH COUNTDOWN + ASCENT EVENTS
Pre-Launch Timeline
Countdown milestones to liftoff
Pre-Launch Timeline
Countdown milestones to liftoff
Final review of all systems, weather, and range safety. GO/NO-GO decision for propellant loading.
Official countdown clock starts. Ground systems power-up sequence initiated.
All non-essential personnel evacuate the pad area. Hazardous operations zone established.
Liquid oxygen and liquid hydrogen loading into SLS core stage. Over 2.6 million liters of cryogenic propellant.
Flight crew awakened at Kennedy Space Center crew quarters. Final medical checks and meal.
Astronauts don Advanced Crew Escape Suits (ACES) — the iconic orange launch-entry suits.
Crew walks out of Neil Armstrong Operations & Checkout Building. Astrovan II drives to Launch Pad 39B.
All four astronauts board the Orion spacecraft. Seats configured, comm checks, survival kit verification.
Orion side hatch closed and sealed. Cabin pressure leak check to verify spacecraft integrity.
Terminal countdown sequence begins. Final system checks, range clear for launch.
Launch director polls all stations for final GO/NO-GO. Artemis Launch Director confirms GO for launch.
Orion spacecraft switches to internal battery power. Ground umbilicals prepared for disconnect.
Ground Launch Sequencer takes over. Automated final checks: hydraulics, engine gimbal, flight termination system.
RS-25 engines at full thrust, SRB ignition, hold-down bolt separation. SLS clears the tower. GO ARTEMIS!
Launch & Ascent
Liftoff through Translunar Injection
SLS clears the tower at Launch Pad 39B. 8.8 million pounds of thrust.
Twin solid rocket boosters jettisoned after burning 1.6 million kg of propellant each.
Launch Abort System and protective panels jettisoned. Orion spacecraft exposed.
Main Engine Cutoff — four RS-25 engines shut down after consuming 2.7 million liters of propellant.
SLS core stage separates. Now relying on the Interim Cryogenic Propulsion Stage (ICPS).
Single RL-10B-2 engine of the ICPS fires for orbital insertion burn.
Parking orbit achieved at ~185 km x 1,800 km. Systems checkout begins.
Translunar Injection burn. ICPS fires again to accelerate Orion to Earth escape velocity.
Orion separates from spent ICPS. Solar arrays unfurl. Crew begins 10-day journey.