The invention discloses a vector magnetic nozzle used for electric propulsion. The vector magnetic nozzle is composed of a permanent magnet arranged in front of a plasma flame-spraying nozzle and a plurality of non-concentric coils which are arranged at the back of the nozzle and form a dipole field. The permanent magnet and the non-concentric coils form a double-magnetic mirror tube so that plasmas can be in reciprocating motion in the double-magnetic mirror tube. The plasmas are heated in effect of ion cyclotron wave resonance under current modulation of the non-concentric coils. Proportion of current on the plurality of non-concentric coils when the plasmas are released from the magnetic nozzle is adjusted so that the vector direction of an external magnetic field of the plasma flame-spraying nozzle of a propeller deviates from the central axis of the propeller so as to guide the flow direction of external plasmas and further to change the thrust vector direction of the propeller. The vector magnetic nozzle can greatly reduce the quantity of the propellers of an attitude control system through vector propulsion, simultaneously greatly improves reliability of the attitude control system, enables vertical speed of the plasmas to be converted to parallel speed, improves parallel flow rate of external flow plasmas, and achieves the purpose of increasing thrust.