The invention discloses an
electromagnetic power thruster which comprises an
ionization section, an accelerating section and a
neutralization jet section. The thruster is characterized in that the
ionization section is composed of a
graphite electrode pipeline (2) which is connected with a
tail gas jet port end of a micro
rocket engine (1); the accelerating section comprises a weak
electrode pipeline (4) and an enhancement
electrode plate (9) on the outer periphery of the weak electrode pipeline (4), and the weak electrode pipeline (4) penetrates through an annular channel formed by an outer cylindrical
magnet (5) and an inner cylindrical
magnet (6); the
neutralization jet section comprises a
cathode ray pipe (8) installed on the outer side of the weak electrode pipeline (4) , a front
magnetism-isolating sleeve (3) is arranged between the
ionization section and the accelerating section, and a rear
magnetism-isolating sleeve (7) is arranged between the accelerating section and the
neutralization jet section. The
electromagnetic power thruster is simple in structure and low in manufacturing cost, energy is saved, the
specific impulse and the thrust-to-
power ratio can be adjusted at will according to requirements, the single equipment can bear high power, and large thrust force can also be obtained.