Low-speed free-flight stability and drag characteristics of radially vented parachutes /
by Sanger M. Burk, Jr.

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Main Author
Burk, Sanger M.
Related Names
Langley Research Center.
United States. National Aeronautics and Space Administration.
Language(s)
English
Published
Washington, D.C. : NASA : 1964.
Subjects
Drag (Aerodynamics) > Testing.
Parachutes > Aerodynamics > Testing.
Summary
A drop-test investigation has been conducted to determine the stability and drag characteristics of radially vented (duplex) parachutes. Parachutes of two different designs were tested: a large parachute with high geometric porosity and a small parachute with low geometric porosity designed for the same descent velocity with the same load. The results of the tests show that the large high-porosity duplex parachute was very stable in descent, oscillations averaging about [plus-or-minus]3.4⁰; and the average drag coefficient based on the total canopy area and based on the fabric area alone were approximately 0.38 and 0.55, respectively. The small, low-porosity duplex parachute was also very stable in descent, oscillations averaging about [plus-or-minus]4.5⁰; and the average drag coefficients based on the total canopy area and based on the fabric area alone were approximately 0.62 and 0.79, respectively. The oscillations for the cluster of three solid flat circular parachutes, tested for comparison purposes, were [plus-or-minus]7.1⁰. The average drag coefficients based on the total canopy area and the fabric area alone were approximately 0.64 and 0.65, respectively.
Note
"March 1964"--Cover.
"National Aeronautics and Space Administration"--Cover.
"NASA Technical Note NASA TN D-2271"--Cover.
"Technical Film Supplement L-817 available on request."
"Langley Research Center Langley Station, Hampton, Va."
This work is part of the library's "Parachute History Collection", donated by the Deutsches Zentrum für Luft- und Raumfahrt e.V. Institut für Flugsystemtechnik, through the American Institute of Aeronautics and Astronautics Aerodynamic Deceleration Systems Technical Committee.
Physical Description
15 [2] p. : ill. ; 28 cm.
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