Once NASA’s Artemis II SLS (Space Launch System) rocket and Orion spacecraft arrived at the Vehicle Assembly Building (VAB) Feb. 25, technicians immediately began addressing why the flow of helium to the SLS upper stage was interrupted as engineers were reconfiguring the rocket following a successful wet dress rehearsal on Feb. 21.

To make the repairs, teams are installing two sets of internal access platforms inside the launch vehicle stage adapter and must remove thermal blankets that cover the area they are interested in – a point on the rocket’s interim cryogenic propulsion system, or upper stage. The area provides connections for multiple umbilicals, including tubing used to fill the upper stage with helium. Helium is used to maintain proper environmental conditions, and to pressurize the stage for flight.

A section of a rocket seen with multiple lines, or umbilicals, connecting it to eqiupment on a tower.
The interim cryogenic propulsion stage has two umbilicals. The highest, smaller ICPS forward plate includes a liquid hydrogen vent and environmental control system air line. The lower, larger aft plate supplies liquid hydrogen, liquid oxygen, and includes a helium quick disconnect and hazardous gas sensing.
NASA

Engineers have narrowed the issue preventing the helium flow to two potential components: a seal on the tubing’s quick disconnect and a check valve on the other end of that tubing.

While the rocket and spacecraft are in the VAB, teams also will install new batteries for the SLS’s upper stage, core stage, and solid rocket boosters, as well as retest its flight termination system and avionics and control systems.

The Orion spacecraft’s launch abort system batteries will be recharged, and engineers may refresh some of the stowed items inside the crew module.

A close view of a section of a rocket with many black lines, or umbilicals, coming out of the side.
Shown is a mated flight and ground plate for the SLS (Space Launch System) core stage’s liquid hydrogen tail service mast umbilical. The quick disconnect device sits between these interface plates once the umbilicals are connected and provide access for flowing propellant into the core stage’s fuel tank. The tail service mast umbilical connects from the zero-level deck on the mobile launcher to the SLS (Space Launch System) rocket core stage aft section and provide liquid oxygen and liquid hydrogen fluid lines and electrical cable connections to the SLS core stage engine section to support propellant handling during prelaunch operations.
NASA

Engineers have optimized planned work in the VAB, and much of the work to come can be done in parallel. Pending the outcome of data reviews, repair efforts, and how the schedule comes to fruition in the coming days and weeks, the Artemis II Moon rocket will roll back to Launch Pad 39B in time for April launch opportunities.

Teams Begin Artemis II Repairs in Vehicle Assembly Building