The invention discloses a
solid-liquid
rocket engine igniter and a head wire-outgoing method thereof, wherein the igniter comprises an igniter box body, an igniter thread ring, and an ignition
powder. The igniter box body is threaded to the igniter thread ring, is sealed by a sealing ring, with an annular cavity for filling the ignition
powder being formed therein. The head wire-outgoing method of the
solid-liquid
rocket engine igniter comprises the following steps: employing an igniter sealing head for being threaded to an igniter
adaptation sleeve; and threading the igniter
adaptation sleeve to an injection panel; inserting one end of an igniter lead wire into an ignition material of the ignition
powder; leading out the lead wire from an ignition hole of the igniter box body; and leading the lead wire outside the engine through a wire hole of the igniter box body, an inner hole of the igniter
adaptation sleeve, and the igniter sealing head. The
solid-liquid
rocket engine igniter has the
advantage of reasonable in structure; and the head wire-outgoing method thereof has the advantages of greatly reducing the length of the igniter lead wire, avoiding the breakage of the igniter lead wire after the igniter is working, reducing the wiring difficulty of the igniter, and increasing the reliability of the igniter.