A laser chamber of a discharge-excitation-type gas laser apparatus may include a container which contains laser gas therein; a pair of discharge electrodes arranged in the container; a cross flow fan configured to supply the laser gas to a discharge space between the discharge electrodes, the cross flow fan including a rotation shaft with which the cross flow fan rotates in a predetermined rotation direction and a plurality of blades, each longitudinal direction of which is parallel to an axial direction of the rotation shaft; and a stabilizer arranged outside a rotation trajectory of the cross flow fan, and arranged such that a difference between a maximum position and a minimum position of an end portion in the rotation direction on a side opposite to the rotation direction is larger than 0 and is smaller than an interval of two blades adjacent to each other among the plurality of blades.

A multi-pass coaxial molecular gas laser is described in both symmetrical and asymmetrical configuration. An anode vessel receives lasing gas and the gas flows through one or more plasma channels to a cathode vessel which receives the gas and redirects it in the closed system. A second anode vessel may alternatively be provided to double length of the plasma channel and increase surface area exposure of the optical beam to the energized gas. Non-laminar gas flow may be created using spiral nozzles at the entrance of the optical resonator.

A multi-pass coaxial molecular gas laser is described in both symmetrical and asymmetrical configuration. An anode vessel receives lasing gas and the gas flows through one or more plasma channels to a cathode vessel which receives the gas and redirects it in the closed system. A second anode vessel may alternatively be provided to double length of the plasma channel and increase surface area exposure of the optical beam to the energized gas. Non-laminar gas flow may be created using spiral nozzles at the entrance of the optical resonator.

Apparatus and methods relating to a gas flow laser are disclosed herein. The gas flow laser includes an eccentrically aligned inner casing within a cylindrical or oval outer shell thereby creating a narrow gas flow path in which the speed of the gas flow may approach sonic or supersonic speeds. An optical resonator is within the narrow gas flow path, and one or more diffusers are located downstream of the optical resonator to improve operating efficiency of the gas flow laser.

Apparatus and methods relating to a gas flow laser are disclosed herein. The gas flow laser includes an eccentrically aligned inner casing within a cylindrical or oval outer shell thereby creating a narrow gas flow path in which the speed of the gas flow may approach sonic or supersonic speeds. An optical resonator is within the narrow gas flow path, and one or more diffusers are located downstream of the optical resonator to improve operating efficiency of the gas flow laser.