Abstract: A combined cooling, heating and power (CCHP) system for extravehicular activity (EVA) space suit is proposed in this paper. The CCHP system mainly consists of a proton exchange membrane fuel cell (PEMFC), a heat driving cooling device, a metal hydride hydrogen storage device and a radiator. A Power Supply Priority scheme is proposed for the CCHP system in order to match both the power supply and the cooling request. Based on the PSP scheme, the operation state parameters and the mass of the CCHP system are calculated under a typical working condition. Influences of the PEMFC's working temperature, the current density and the pressure on the system mass and the expendable material loss are analyzed. The results show that the mass of the EVA space suit CCHP system is acceptable, and the expendable material loss is much less than that of the water sublimator/storage battery scheme. Lowering the PEMFC working temperature and pressure, or raising the PEMFC's current density, would lead to a lighter system and less expendable material loss.