Yes, but most of the time LOX and LH2 are low-pressure, thin walled structures. The fuel and oxidizer are pressurized using turbopumps. The External Tank of the Shuttle was thin-walled and collapsed on itself during re-entry, leaving a debris field in the Atlantic.
Now, if there are no turbopumps involved, then you would need a much thicker tank, as the fuel and oxidizer would be under high pressure.
As would happen on a satellite maneuvering system where the propellant would be under pressure with no or minimal venting for extended periods of time ( like years) requiring a very solid walled tank that may or may not be exposed to direct sunlight depending on the design of the satellite. Remember - the life of a satellite has orbit maintenance burns , or the ability to change orbit ( for surveillance missions) as part of it’s design.