CEAS Space Journal

A porous flow control element for pulsed plasma thrusters
Depressurization solutions of vented enclosures during launch
European Space Agency’s launcher multibody dynamics simulator used for system and subsystem level analyses
Investigations on the thermal behaviour of CMC-based leading edges in hypersonic arc jet flows
Methodologies for launcher–payload coupled dynamic analysis
Weak stability boundary transfer to the Moon from GTO as a piggyback payload on Ariane 5