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Basic relationships for LTA technical analysisAn introduction to airship performance is presented. Static lift equations are shown which, when combined with power requirements for conventional airships, allow parametric studies of range, payload, speed and airship size. It is shown that very large airships are required to attain reasonable speeds at transoceanic ranges.
Document ID
19760007938
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ausrotas, R. A. (Massachusetts Inst. of Tech. Cambridge, MA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Proc. of the Interagency Workshop on Lighter than Air Vehicles
Subject Category
Aircraft Design, Testing And Performance
Accession Number
76N15026
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19760007927Collected WorksProceedings of the Interagency Workshop on Lighter than Air Vehicles
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