The invention provides a piezoelectric micro-thruster comprising an air inlet (1), a housing (2), a power interface (3), a filter (4), a return spring (5), a valve core (6), a piezoelectric stack (7), a
washer spring (8), a
valve seat (9), a seal ring (10), an adjusting ring (11), a base (12) and a
nozzle (13). In the case of power-off, the surface of the valve core (6) is tightly attached to the surface of the
valve seat (9) and the surface of the adjusting ring (11), and the piezoelectric micro-thruster is off; in the case of power-on, the piezoelectric stack (7) deforms to drive the valve core (6) to move, the surface of the valve core (6) separates from the surface of the
valve seat (9) and the surface of the adjusting ring (11), the piezoelectric micro-thruster is on and generates thrust. The sealing parts, such as the valve core (6), the valve seat (9) and the adjusting ring (11), are all made of
metal, thus the piezoelectric micro-thruster is
metal sealed. The piezoelectric micro-thruster is short in
response time, continuously adjustable in thrust, low in
power consumption and long service, meets the strict requirements of miniature satellites and
missile precision guides for micro-thrust systems and is light in weight and small in size, and more weight and space are saved for the miniature satellites.