I'm trying to figure out whether a centrifugal flow compressor (like the type used on early turbojets) which has only one main moving part be suitable for use in a phase-change cooler? If not that, how about an axial flow compressor (as used in modern turbojets)? I'm thinking it might provide some advantages over reciprocating or scroll compressors, mainly in reducing vibration severity. Am I looking in the wrong place?