Safe launching method for small missile

The invention discloses a safe launching method for small missiles, which adopts the overall schemes of barrel type launching, low initial speed, common nozzle multi-pulse power, micro-smoke propellant, gas vane thrust vector control, observation and aiming control device man-machine ring design and the like, and ensures a safe distance through a multi-pulse mode in a micro-sound, micro-smoke, micro-flame and micro-backseat'four-micro 'soft launching mode. Thrust vector control is carried out through a gas vane; the initial disturbance of the muzzle is overcome, and the safety risk caused by short-distance falling of the missile is eliminated; when the engine 2 is subjected to pulse ignition, the missile is rapidly subjected to posture adjustment, and objects ejected by the engine are prevented from hurting a shooter; the face of a shooter is protected through the man-machine ring design of the observing and aiming control device, and safe launching of small missiles is achieved. The four-micro soft launching