The invention provides a
near space jet propulsion system based on a fuel
cell and a propulsion method thereof, and belongs to the technical field of
near space propulsion. The
system comprises an inner shell, an outer shell, a fluid conveying
system, a
motor system, a porous structural body, a high-speed molecular-level rotating shaft pump, a precooler, a
liquid hydrogen tank, a
liquid oxygen tank, a high-temperature
proton exchange membrane fuel
cell, a
tail gas collecting and electrolyzing device, a pressure stabilizing chamber, a direct-current conversion
control system and an expansion cavity, the invention discloses a flexible solar panel and a
plasma electromagnetic jet generator. The system integrates
hybrid power supply of a high-temperature
proton exchange membrane fuel
cell and a flexible solar panel, and is coupled with a
tail gas collection
electrolysis device to realize in-situ regeneration of an
oxyhydrogen working medium; main thrust is generated through the
plasma electromagnetic jet generator, multi-mode propulsion is formed in cooperation with the distributed electric propulsion unit, the bottlenecks of unstable
combustion,
high carbon emission, short endurance and the like in a rarefied air environment are broken through, and zero-carbon-emission, long-endurance and high-reliability operation of the
near space aircraft is achieved.