Igniter and fuse integrated structure of rocket engine

The utility model relates to a rocket engine igniter and fuze integrated structure, which structurally comprises a front fuze body and a rear fuze body which are oppositely combined together, a rotor seat is arranged in a cavity formed by the front fuze body and the rear fuze body, a rotor is arranged on the rotor seat, a connecting screw is arranged on the rear fuze body, and the front fuze body and the rear fuze body are integrally connected. An electric ignition tube is arranged on the connecting screw, a safety mechanism is connected to the rear fuse body and the connecting screw in a penetrating mode, and the safety mechanism is used for limiting rotation of the rotor. The igniter and the fuze of the rocket projectile are combined into a whole, the whole is installed on the rocket projectile body, the functions of ignition and fuze are achieved, the overall size is small, the structure is simple, and the production cost is low. 本实用新型涉及一种火箭发动机点火具与引信一体结构，其结构包括对合在一起的前引信体和后引信体，在所述前引信体和所述后引信体形成的腔体内设置有转子座，在所述转