A wing deployment and locking system comprising, - a first wing and a second wing, forming an aerodynamic surface. - a first spring housing having first one-way clutches at each end through which the first spring housing can make only rotational motion about a first spring retainer and a first bearing housing axis to rotate the first wing, - a pre-stressed first machined spring that is fixed to the first spring housing by means of a first spring pin on one side and the first spring retainer on the other, - at least two first lock springs and at least two first lock pins, that are positioned inside a casing, - at least two lock pin housings positioned on the first spring housing such that at least two first lock pins located inside the casing can slide separately into the lock pin housings by means of the first lock springs located behind the said lock pins when the first wing is in a fully deployed position, - an actuator mechanism that enables the first machined spring, which is torsionally loaded when the first wing is in an undeployed state, to be released, which allows the first spring housing to be rotated, - at least two casing protrusions located on the casing, - at least two first spring housing recesses having a formed surface, which are positioned on the first spring housing so as to match separately with the at least two casing protrusions located on the casing when the first wing is in the fully deployed position, - a second spring housing having second one-way clutches at each end through which the second spring housing can make only rotational motion about a second spring retainer and a second bearing housing axis to rotate the second wing, - a pre-stressed second machined spring that is fixed to the second spring housing by means of a second spring pin on one side and second spring retainer on the other, - at least one second lock spring and at least one second lock pin, that are located inside the second bearing housing, - a third cover that holds the second lock spring in the compressed position, - a second bearing housing protrusion located on the second bearing housing and a second spring retainer protrusion located on the second spring retainer, - two second spring housing recesses having a formed surface, which are positioned at both ends of the second spring housing so as to match separately with the second spring retainer protrusion and the second bearing housing protrusion when the second wing is in the fully deployed position. - a first wing and a second wing, forming an aerodynamic surface. - a first spring housing having first one-way clutches at each end through which the first spring housing can make only rotational motion about a first spring retainer and a first bearing housing axis to rotate the first wing, - a pre-stressed first machined spring that is fixed to the first spring housing by means of a first spring pin on one side and the first spring retainer on the other, - at least two first lock springs and at least two first lock pins, that are positioned inside a casing, - at least two lock pin housings positioned on the first spring housing such that at least two first lock pins located inside the casing can slide separately into the lock pin housings by means of the first lock springs located behind the said lock pins when the first wing is in a fully deployed position, - an actuator mechanism that enables the first machined spring, which is torsionally loaded when the first wing is in an undeployed state, to be released, which allows the first spring housing to be rotated, - at least two casing protrusions located on the casing, - at least two first spring housing recesses having a formed surface, which are positioned on the first spring housing so as to match separately with the at least two casing protrusions located on the casing when the first wing is in the fully deployed position, - a second spring housing having second one-way clutches at each end through which the second spring housing can make only rotational motion about a second spring retainer and a second bearing housing axis to rotate the second wing, - a pre-stressed second machined spring that is fixed to the second spring housing by means of a second spring pin on one side and second spring retainer on the other, - at least one second lock spring and at least one second lock pin, that are located inside the second bearing housing, - a third cover that holds the second lock spring in the compressed position, - a second bearing housing protrusion located on the second bearing housing and a second spring retainer protrusion located on the second spring retainer, - two second spring housing recesses having a formed surface, which are positioned at both ends of the second spring housing so as to match separately with the second spring retainer protrusion and the second bearing housing protrusion when the second wing is in the fully deployed position.