NASA NTRS · 19700039294
Development of an extremely lightweight, high- altitude decelerator
Abstract
Parachute design for decelerating upper atmosphere rocket probes at high altitudes, using high drag coefficients in Stokes flow regime
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Niederer, P. G.. 1969-11-01. Development of an extremely lightweight, high- altitude decelerator. https://ntrs.nasa.gov/citations/19700039294
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