A controllable launch system comprises a housing (1), said housing containing at least one closed-type launch module (2), a control unit (3), at least one power element (4), at least indicator element (5) for indicating the status of the launch module, and at least one indicator element (5) for indicating the status of the power element. The closed-type launch module consists of a housing (8) containing: a projectile (9), a cut-off piston (10), a propellant (11), and a firing element (12). The at least one closed-type launch module, the control unit, the at least one power element, the at least one indicator element for indicating the status of the launch module and the at least one indicator element for indicating the status of the power element are designed to be controllable by means of a wired connection and/or via a radio channel.
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