An airship is presented having a plurality of resilient gas bags and gas containers, a straight fuselage tubular hull, with an inner air passageway and propulsion system located therein, and, connecting air inlet, and outlet funnels fore, and aft, with air deflector cones axially positioned therein. The ship also contains propulsion, reverse, and directional rocket thrusters, in addition to typical airship components.
Airship with internal propulsion system
2016-03-29
Patent
Elektronische Ressource
Englisch
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