Complete Timeline of the Artemis II Mission: Download the Calendar
Artemis II Mission Milestones: Minute by Minute
βοΈ Propellant Load
Cryogenic liquid oxygen (LOX) and liquid hydrogen (LH2) loading begins in the SLS core stage.
πΆββοΈ Crew Walkout
Astronauts exit the O&C building and board the Astrovan transport vehicles to the pad.
π§βπ Capsule Ingress
The crew arrives at the "White Room" on the launch tower and begins boarding Orion.
πͺ Hatch Closure
Orion's side hatch is closed and sealed. Leak checks are underway.
β±οΈ Terminal Countdown
The Launch Director gives the final "GO". Automated countdown initiates.
π» Auto Sequence Hand-off
Ground systems hand off control to SLS flight computers. Ignition sequence begins.
π Liftoff (Ascent)
RS-25 engines and solid boosters come to life. Official start of the MET clock.
π¬οΈ Cabin Depress (DFTO 3, 2)
Spacesuit seal test. Cabin pressure is intentionally reduced.
π₯ Perigee Raise Maneuver (ICPS PRM)
The upper stage fires engines to stabilize initial orbit 50 minutes into flight.
π» Pre ARB C/Os
Preliminary systems checkouts prior to the apogee raise maneuver.
π₯ Apogee Raise Burn (ARB TIG)
Burn scheduled at 0/01:47 to elongate the orbit elliptically to gain altitude.
π§βπ Doff Survival Suits (OCSS)
Astronauts take off the heavy orange Orion Crew Survival System suits.
π Orion/ICPS Spring Sep
Orion spacecraft physically disconnects from the upper stage via springs at 3 hours 23 minutes.
π°οΈ Prox Ops Demo (Orion USS)
At 0/04:51, astronauts test manual controls flying in proximity to the discarded stage.
ποΈ ICPS Disposal Burn
The ICPS stage fires its engine at 0/05:02 to move to a safe graveyard orbit.
βοΈ Solar Panel Deploy (SPL)
At 0/05:27, the European Service Module deploys its four solar arrays.
π· Dock Cam Bearing
Optical camera bearing alignment scheduled at 0/06:00.
π² Cabin Config
Organization of supplies inside the capsule.
ποΈ PAD / PMC Checks
Private medical conference (PMC) and Preliminary Advisory Data review.
π€ First Sleep Cycle (4 hrs)
Brief 4-hour crew rest after the launch day.
π‘ OpComm Activation
Initial activation of the laser optical communications system at 0/10:06.
π₯ Orion Perigee Raise Burn (PRB)
Orion fires its main engine at 0/13:30 to adjust final orbit before jumping to the Moon.
π OpNav C/O
Optical navigation system checkouts at 0/14:15.
π€ Second Sleep (4.5 hrs)
Main 4.5-hour sleep cycle to prepare for lunar injection.
π TLI Conf (Go/No-Go)
Critical conference to authorize leaving Earth orbit. This stage is crucial to ensure all systems are ready for the jump to the Moon.
πͺ Exercise Test
Test of the cabin's resistive exercise equipment.
π¬οΈ ECLSS CO2 Monitor DFTO
Flight test of the life support system's carbon dioxide monitor.
π οΈ Asc Bracket Uninstall
Uninstalling the docking camera and ascent brackets to free up space.
π Trans-Lunar Injection (Orion TLI)
Main burn at 01/01:08:42. The ship leaves Earth heading for the Moon.
π² Meal
Meal routine for the crew.
ποΈ PAO Event
Public Affairs Office connection.
π Window Inspect
Detailed visual inspection of capsule windows.
π οΈ Dual Cam Bracket Install
Installation of the dual camera bracket for deep space operations.
π€ Deep Space Sleep (8.5 hrs)
Standard 8.5-hour rest cycle.
π Thermal Inspection (CM/SM Survey)
Use of cameras at 01/14:00 to scan the heat shield for damage.
π‘ OpCom ANU Demo
Advanced link demonstration of the optical communications system.
π οΈ Outbound Correction (OTC-1)
First Outbound Trajectory Correction burn scheduled at 02/01:08:42.
π©Ί CPR Demo
Astronauts perform a Cardiopulmonary Resuscitation (CPR) demo in microgravity.
π‘ SAT Mode Test
Test of the satellite communications mode.
βοΈ Med Kit
Review of the onboard medical kit.
π Lunar Cab
Cabin configuration for lunar proximity operations.
π DSN Emergency Comms
Emergency link test (EMER Comm DFTO-EM2-22) with the Deep Space Network.
ποΈ CSA PAO Event
Exclusive link with the Canadian Space Agency (CSA).
π· Dock Cam Misalign Test
Test DFTO-EM2-03 forcing a virtual misalignment of the optical camera.
π€ Sleep Cycle (FD03)
8.5 hours rest.
π οΈ Outbound Correction (OTC-2)
Second trajectory correction scheduled at 3/01:08:42.
π§ͺ Min ECLSS DFTO
Minimum environmental systems test (DFTO EM2-18).
π§ Start 24h Acoustic DFTO
Starts a continuous ambient noise measurement test (EM2-7).
π· Dock Cam & Bracket Install
Installation of additional optical tools.
π§ NAV FTO
Navigation flight objectives test at 03/07:00 (EM2-223).
π€ Early Sleep Cycle
8.5-hour rest shifted 45 minutes earlier in preparation for the Moon.
π οΈ OTC-3
Third and final powered correction (4/04:29:52) before lunar influence.
π Lunar SOI Entry
Orion crosses the Moon's gravitational boundary at 4/06:38.
π§ End 24h Acoustic DFTO
24-hour ambient recording ends.
π¬οΈ Vent to 10.2 psi
Cabin pressure is equalized to reduced levels.
π· Dock Cam Misalign Test
Test DFTO-EM2-03 prior to approaching the lunar surface.
π€ Sleep Cycle (Pre-flyby)
Rest shifted 1 hour earlier; the last before the encounter.
π Lunar Close Approach
Closest point on the far side of the Moon at 5/00:29:59.
π Max Earth Distance
The furthest point from Earth at 5/00:35.
π Apollo Record
The crew breaks the historical distance record.
π Lunar Obs
Visual observations of the Moon's surface following the flyby.
π Post-Lunar Survey
External review of the heat shield at 05/12:30.
π Lunar SOI Exit
Exit from the Moon's gravitational influence at 5/18:53.
π€ Deep Sleep (9.5 hrs)
Extended 9.5-hour sleep shift pushed 1 hour later.
π οΈ Return Trajectory Correction RTC-1
First Return Trajectory Correction burn scheduled at 6/01:29:52.
π· Dock Cam WW Dump
Download of data captured by flight objectives (Dock Cam WW Dump FTO).
π· Dock Cam Misalign
Continuation of misalignment tests on the return journey.
β’οΈ Rad Shelter Demo
Test construction of the solar storm radiation shelter using internal storage.
π» FCS Checkouts
Tests of the Flight Control System (FCS) computers at 7/17:30.
π Modal Survey DFTO
Inspections of structural dynamics and vibrations of the crew module (EM2-27).
π§ Urine Venting Test
Expulsion test into deep space (DFTO EM2-26).
π¬οΈ Repress to 14.7 psi
Restoration of cabin pressure to standard levels.
π§βπ Suit Up (OIG Don)
Astronauts don orange survival suits preparing for landing.
π οΈ Return Trajectory Correction RTC-2
Fine tuning scheduled at 8/04:29:10 to secure the atmospheric corridor.
π Entry Stow
Final stowage of all loose cabin items.
π οΈ Return Trajectory Correction RTC-3
Final ballistic adjustment straight towards the Pacific Ocean at 8/20:29:10.
π Module Separation (CM/SM Sep)
The European Service Module is discarded at 09/01:09 to burn up in the atmosphere.
π§ +X Leak Detection
Final leak detection test (DFTO) prior to atmospheric entry.
π₯ Entry Interface
Capsule hits the atmosphere at Mach 32 at 09/01:29.
π Splashdown
Splashdown in the waters of the Pacific Ocean at 09/01:42:48. Mission accomplished!
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