A controllable launch system comprises a housing (1) containing at least one closed-type launch module (2) and a control unit (3), wherein the launch module consists of a housing containing a projectile, a cut-off piston, a propellant and a firing element, and the control unit is designed to be capable of generating commands addressed to the at least one closed-type launch module. The system also comprises at least one power element (4) mounted inside the housing of the system and/or connected to the housing of the system by a wired connection, at least indicator element (5) for indicating the status of the closed-type launch module, and at least one indicator element (5) for indicating the status of the power element, wherein the at least one indicator element for indicating the status of the closed-type launch module and/or the at least one indicator element for indicating the status of the power element is mounted inside the housing of the system and/or is connected to the housing of the system by a wireless connection and/or via a radio channel.
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