NASA NTRS · 19760007938
Basic relationships for LTA technical analysis
Abstract
An 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.
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Ausrotas, R. A.. 1975-01-01. Basic relationships for LTA technical analysis. https://ntrs.nasa.gov/citations/19760007938
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