
SLS LVSA for Artemis IV
The agency intends to spare up their only left ICPS for Artemis IV and use a 1:1 dummy spacer on Artemis III.
Now, if they fly the spacer on Artemis III, they will need an LVSA to connect it to the core stage. But if they use it on Artemis III, what will they use to connect their last ICPS to the core stage of Artemis IV?
I‘m assuming they have only made three LVSA for three ICPS stages, so what am I missing? I couldn’t find any answer to my question elsewhere, so I hope it has its place here