Space Launch System The Space Launch System (SLS) is a
super-heavy-lift launcher used to launch the Orion spacecraft from Earth to a trans-lunar orbit. This mission's
core stage will use
RS-25 engines E2044, E2050, E2051, and E2063. This will potentially be the first mission to use the standardized configuration of the SLS, with a
Centaur V upper stage in place of the
Interim Cryogenic Propulsion Stage (ICPS) flown on the previous SLS launches. However, Artemis IV may instead use the ICPS if NASA elects to not use an ICPS on the
Artemis III mission to test the HLS landers in Earth orbit.
Orion Multi-Purpose Crew Vehicle Orion is the
crew transport vehicle used by all Artemis missions. It comprises the Orion Crew Module and the European Service Module and will transport the crew from Earth to Lunar orbit, dock to the lander, and return them to Earth. The
European Service Module (ESM) for Artemis IV, ESM-4, was delivered to NASA from the Airbus facility in
Bremen, Germany, in December 2025.
Human Landing System Artemis IV will use one of NASA's two Human Landing System lunar landers: SpaceX's Starship HLS or Blue Origin's Blue Moon. The choice of lander depends on the results of the low-Earth orbit rendezvous and docking tests conducted during
Artemis III in mid-2027, as well as each company's readiness to deliver the spacecraft for the mission. == See also ==