A cooling system for landing craft (1), which cools at least one propulsion engine (4) of the landing craft (1) and that comprises a series of cooling liquid circulation conduits (5) and at least one pump (6), and which additionally comprises: - at least one stern cooling liquid inlet (7), disposed on the stern (2) of the landing craft (1), - at least one bow cooling liquid inlet (8), disposed on each side (3, 3') of the landing craft (1), and - at least one valve (9) that enables the passage of the cooling liquid from at least one stern inlet (7), from at least one bow inlet (8) or from at least one stern inlet (7) and at least one bow inlet (8) simultaneously.
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