![\"Image](\"https:\/\/www.nasa.gov\/wp-content\/uploads\/2025\/03\/ksc-20250323-ph-fmx01-0250.jpg?w=2048\")
<\/a><\/figure>For Artemis II, the major sections of SLS remain unchanged \u2013 a central core stage, four RS-25 main engines, two five-segment solid rocket boosters, the ICPS (interim cryogenic propulsion stage), a launch vehicle stage adapter to hold the ICPS, and an Orion stage adapter connecting SLS to the Orion spacecraft. The difference is in the details.<\/p>\n
\u201cWhile we\u2019re proud of our Artemis I performance, which validated our overall design, we\u2019ve looked at how SLS can give our crews a better ride,\u201d said John Honeycutt, NASA\u2019s SLS Program manager. \u201cSome of our changes respond to specific Artemis II mission requirements while others reflect ongoing analysis and testing, as well as lessons learned from Artemis I.\u201d<\/p>\n
Engineers have outfitted the ICPS with optical targets that will serve as visual cues to the astronauts aboard Orion as they manually pilot Orion around the upper stage and practice maneuvers to inform docking operations for Artemis III.<\/p>\n
The Artemis II rocket includes an improved navigation system compared to Artemis I. Its communications capability also has been improved by repositioning antennas on the rocket to ensure continuous communications with NASA ground stations and the U.S. Space Force\u2019s Space Launch Delta 45 which controls launches along the Eastern Range.<\/p>\n
An emergency detection system on the ICPS allows the rocket to sense and respond to problems and notify the crew. The flight safety system adds a time delay to the self-destruct system to allow time for Orion\u2019s escape system to pull the capsule to safety in event of an abort.<\/p>\n
The separation motors that push the solid rocket booster away after the elements are no longer needed were angled an additional 15 degrees to increase separation clearance as the rest of the rocket speeds by.<\/p>\n
Additionally, SLS will jettison the spent boosters four seconds earlier during Artemis II ascent than occurred during Artemis I. Dropping the boosters several seconds closer to the end of their burn will give engineers flight data to correlate with projections that shedding the boosters several seconds sooner will yield approximately 1,600 pounds of payload to Earth orbit for future SLS flights.<\/p>\n
Engineers have incorporated additional improvements based on lessons learned from Artemis I. During the Artemis I test flight the SLS rocket experienced higher-than-expected vibrations near the solid rocket booster attachment points that was caused by unsteady airflow.<\/p>\n
To steady the airflow, a pair of six-foot-long strakes flanking each booster\u2019s forward connection points on the SLS intertank will smooth vibrations induced by airflow during ascent, and the rocket\u2019s electronics system was requalified to endure higher levels of vibrations.<\/p>\n
Engineers updated the core stage power distribution control unit, mounted in the intertank, which controls power to the rocket\u2019s other electronics and protects against electrical hazards.<\/p>\n
These improvements have led to an enhanced rocket to support crew as part of NASA\u2019s Golden Age of innovation and exploration.<\/p>\n
The approximately 10-day Artemis II test flight is the first crewed flight under NASA\u2019s Artemis<\/a> campaign. It is another step toward new U.S.-crewed missions on the Moon\u2019s surface that will help the agency prepare to send the first astronauts \u2013 Americans \u2013 to Mars.<\/p>\n https:\/\/www.nasa.gov\/artemis<\/a><\/p>\n Jonathan DealNews Media Contact<\/h2>\n
Marshall Space Flight Center, Huntsville, Ala.\u00a0
256.631.9126
jonathan.e.deal@nasa.gov<\/a><\/p>\nShare<\/h2>\n<\/p><\/div>\n