Abstract: The use of thrusters at the bow and stern of an airship for control of the direction, attitude, and orientation of such an airship is described. The thruster utilizes an electric motor or a gas turbine for power. In the electric motor embodiment, the motor utilizes two contra-rotating rotors which each drive a separate and contra-rotating propeller to generate the controlling jet of air. Thrusters are arranged in pairs at the top, bottom, and each side of the bow and stern of the airship. Lifting thrusters directed downwardly and located above the longitudinal extent of the hull are provided to augment the static lift capability of the airship when under heavy load.

Abstract: A method of assembling a metal-clad rigid airship hull and apparatus for use in the assembly is disclosed. The apparatus is a rotating cradle consisting of an endless belt extending around and suspended between motor-driven cylinders. The cradle is rotated to provide angular positioning of hull surfaces of the airship at specific work locations. The bow and stern of the airship are assembled in a vertical position and, upon completion, are hoisted by a crane or sling to the horizontal position and attached to the main section of the airship hull structure utilizing the rotating cradle.

Abstract: A construction of the external skin of the hull of a metal-clad airship utilizing sections of hull plating of different thickness to connect the sheets or gores of the plating of the main portion of the hull to the base skin of structural members, such as external longerons and internal frame members.