Abstract: A launch system including a tower having a platform affixed to the apex of the tower; at least one rotary ring, the at least one rotary ring including an inner-edge and an outer-edge circumscribing an inner-radius and an outer-radius of the at least one rotary ring respectively. A coupling-mechanism is configured to mate the inner-edge of the at least one rotary ring to the outer-edge of another of the at least one rotary ring. A gyroscopic stabilization device is configured to maintain a planar-relation between more than one rotary rings. A transverse-channel spans a diameter of the at least one rotary ring defining a path for cargo to traverse the diameter of the at least one rotary ring. The launch system is configured to utilize a centrifugal force generated by rotating the at least one rotary ring to launch a cargo into atmosphere.

Abstract: A launch system including a tower having a platform affixed to the apex of the tower; at least one rotary ring, the at least one rotary ring including an inner-edge and an outer-edge circumscribing an inner-radius and an outer-radius of the at least one rotary ring respectively. A coupling-mechanism is configured to mate the inner-edge of the at least one rotary ring to the outer-edge of another of the at least one rotary ring. A gyroscopic stabilization device is configured to maintain a planar-relation between more than one rotary rings. A transverse-channel spans a diameter of the at least one rotary ring defining a path for cargo to traverse the diameter of the at least one rotary ring. The launch system is configured to utilize a centrifugal force generated by rotating the at least one rotary ring to launch a cargo into atmosphere.