NASA NTRS · 19830014969
Helicopter technology benefits and needs. Volume 1: Summary
Abstract
Present public service helicopter benefits and the potential benefits of an advanced public service rotorcraft (200 knots to 300 knots) are summarized. Past and future public service growth is quantified and assessed and needs, problem areas, and desired vehicle characteristics are defined. Research and technology recommendations are formulated and the costs and benefits of research options are assessed.
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Zuk, J., Adams, R. J.. 1980-07-01. Helicopter technology benefits and needs. Volume 1: Summary. https://ntrs.nasa.gov/citations/19830014969
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