The invention belongs to the technical field of multi-tube grenade launchers, and particularly discloses an ejection mechanism of a multi-tube remote launcher, which comprises an ejection jack seat, a guide part, an ejection jack and an ejection driving part, the ejection
tappet is movably arranged between the two bullet holes in the middle layer, and four mounting arms are arranged on the ejection
tappet in the circumferential direction of the ejection
tappet; the number of the ejection stiles is four, the ejection stiles are correspondingly installed on the four installation arms respectively, the installation positions of the four ejection stiles form four vertexes of a rectangle, three bullet holes are evenly distributed in the outer side of each ejection
stile, and the end, away from the ejection
stile base, of each ejection
stile movably penetrates through the rear linkage and is provided with ejection bullet teeth. Each ejection tooth is configured to synchronously eject
cartridge cases in three
cartridge holes in the outer side of the corresponding ejection jack; and the ejection driving piece is connected to the rear link. According to the ejection mechanism, the limited space under the 323
layout is fully utilized, ejection operation is efficiently and accurately conducted on the
cartridge cases in all the cartridge holes, and the ejection problem under the specific
layout is solved.