The invention provides a refrigerating
system for a Mars in-situ
propellant preparation and storage process, which comprises a gas-liquid separation
storage tank, a compressor, an aftercooler, a heat regenerator, a first
throttle valve, a
carbon dioxide capture module, a
liquid oxygen storage tank, a
liquid methane storage tank and a fan, and is characterized in that the heat regenerator comprises a high-pressure
refrigerant flow channel, a low-pressure
refrigerant flow channel, an
oxygen flow channel and a
methane flow channel;
gaseous oxygen is liquefied in the
oxygen flow channel and then stored in the
liquid oxygen storage tank, and gaseous
methane is liquefied in the
methane flow channel and then stored in the
liquid methane storage tank; the
carbon dioxide capturing module comprises a
refrigerant flow channel and a
carbon dioxide flow channel, a refrigerant of the refrigerant flow channel is used for providing
cooling capacity for carbon dioxide freezing capturing, fluid of the carbon dioxide flow channel is Mars
atmosphere, and the Mars
atmosphere is introduced into the carbon dioxide capturing module through a fan. According to the refrigerating
system, integrated cooling of carbon dioxide capture, methane
liquefaction and
oxygen liquefaction can be achieved, and the complexity of
system configuration is reduced.