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Vehicle concepts and technology requirements for buoyant heavy-lift systemsSeveral buoyant-vehicle (airship) concepts proposed for short hauls of heavy payloads are described. Numerous studies identified operating cost and payload capacity advantages relative to existing or proposed heavy-lift helicopters for such vehicles. Applications involving payloads of from 15 tons up to 800 tons were identified. The buoyant quad-rotor concept is discussed in detail, including the history of its development, current estimates of performance and economics, currently perceived technology requirements, and recent research and technology development. It is concluded that the buoyant quad-rotor, and possibly other buoyant vehicle concepts, has the potential of satisfying the market for very heavy vertical lift but that additional research and technology development are necessary. Because of uncertainties in analytical prediction methods and small-scale experimental measurements, there is a strong need for large or full-scale experiments in ground test facilities and, ultimately, with a flight research vehicle.
Document ID
19810022643
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Ardema, M. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TP-1921
A-8022
Accession Number
81N31185
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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