A swiveling mount for a lightweight missile launcher having a single-use launch tube containing a self-propelled missile, said launch tube being coupleable both mechanically and electrically to a reusable control unit through complementary connectors, said control unit allowing locating a target, firing the missile and/or guiding the missile, said swiveling mount including: • a first support, that can be fixed to a base, equipped with a first articulation suitable for rotating about a vertical axis and for preventing axial movement in the direction of the vertical axis; • a second support attached to the first support by means of at least a second articulation suitable for pivoting about a horizontal axis and for preventing axial movement in the mentioned direction of the horizontal axis; • at least one locking element that allows fixing said first articulation and/or second articulation in a desired angular position; characterized in that the mount furthermore incorporates: • a guided carriage attached to the second support by means of guiding elements that allow a guided movement of said guided carriage with respect to said second support between a disarmed position, in which the launch tube and the control unit of the missile launcher are uncoupled from one another, and an armed position, in which the launch tube and the control unit of the missile launcher are coupled through the mentioned connectors and is ready to be fired; • control unit anchors provided for precisely positioning and firmly and securely fixing the control unit of the missile launcher to the mount; and • launch tube anchors provided for precisely positioning and firmly and securely fixing the single-use launch tube to the mount; wherein the control unit anchors and the launch tube anchors being respectively attached on the second support and on the guided carriage or vice versa, allowing a guided movement of the launch tube anchors with respect to the control unit anchors; and wherein said guided movement of the guided carriage includes, with respect to an axis defined by a firing direction, which is defined by the launch tube, lateral movement and axial movement in the firing direction. • a first support, that can be fixed to a base, equipped with a first articulation suitable for rotating about a vertical axis and for preventing axial movement in the direction of the vertical axis; • a second support attached to the first support by means of at least a second articulation suitable for pivoting about a horizontal axis and for preventing axial movement in the mentioned direction of the horizontal axis; • at least one locking element that allows fixing said first articulation and/or second articulation in a desired angular position; • a guided carriage attached to the second support by means of guiding elements that allow a guided movement of said guided carriage with respect to said second support between a disarmed position, in which the launch tube and the control unit of the missile launcher are uncoupled from one another, and an armed position, in which the launch tube and the control unit of the missile launcher are coupled through the mentioned connectors and is ready to be fired; • control unit anchors provided for precisely positioning and firmly and securely fixing the control unit of the missile launcher to the mount; and • launch tube anchors provided for precisely positioning and firmly and securely fixing the single-use launch tube to the mount;