NASA NTRS · 19660061309
The spinning filamentary disk as a hypersonic decelerator.
Abstract
Flexible uniform-stress truncated disk spinning about central hub for aerodynamic braking useful as reentry decelerator, noting low decelerator weight fractions for wide range of mission parameters
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Kyser, A. C., Macneal, R. H.. 1966-01-01. The spinning filamentary disk as a hypersonic decelerator.. https://ntrs.nasa.gov/citations/19660061309
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