A method for reducing or eliminating “Missile Tip-off Effect” (MTE) of a missile ejected from a canister. The method includes: receiving data of desired canister state in response to a launch command. The method further include perform repeatedly until an MTE control criterion is met: (a) receiving, from a sensor associated with the canister, data of measured canister state, and (b) processing the data of the measured canister state and desired canister state, for outputting data indicative of a command to an actuator associated with the canister for modifying at least the angular position of the canister, thereby reducing or eliminating the (MTE) effect.

The present invention relates to a rocket launching module comprising a base frame (1) comprising at least one rail (2a); a sliding table (3) configured to slide substantially vertically on said rail (2a) when driven by at least one electric linear actuator (11), and a targeting device (4) comprising a turntable (5) on which a pivotable body (6) is mounted, supporting a rocket support portion (7). The sliding table (3) comprises a platform (8) configured to receive the turntable (5) of the targeting device (4).

The present invention relates to a rocket launching module comprising a base frame (1) comprising at least one rail (2a); a sliding table (3) configured to slide substantially vertically on said rail (2a) when driven by at least one electric linear actuator (11), and a targeting device (4) comprising a turntable (5) on which a pivotable body (6) is mounted, supporting a rocket support portion (7). The sliding table (3) comprises a platform (8) configured to receive the turntable (5) of the targeting device (4).

The present invention relates to a rocket launching module comprising a base frame (1) comprising at least one rail (2a); a sliding table (3) configured to slide substantially vertically on said rail (2a) when driven by at least one electric linear actuator (11), and a targeting device (4) comprising a turntable (5) on which a pivotable body (6) is mounted, supporting a rocket support portion (7). The sliding table (3) comprises a platform (8) configured to receive the turntable (5) of the targeting device (4).

The present invention relates to a rocket launching module comprising a base frame (1) comprising at least one rail (2a); a sliding table (3) configured to slide substantially vertically on said rail (2a) when driven by at least one electric linear actuator (11), and a targeting device (4) comprising a turntable (5) on which a pivotable body (6) is mounted, supporting a rocket support portion (7). The sliding table (3) comprises a platform (8) configured to receive the turntable (5) of the targeting device (4).