I am asking this question in a context of feasability of orbital fuel depots.
I understand that cost/kg estimates exist (2-14 k$/kg): What is the current cost-per-pound to send something into LEO? ]), but the post dates back to 2013 and asked for an update on the values. But what about larger masses ie 1 metric ton and more? What would the launching cost be, considering the structural requirements for storing the LOX/LH2?