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Effect of suspension-line viscous damping on parachute opening load amplification.A digital computer program was used to investigate the effects of suspension-line viscous damping on the opening loads of a high-altitude parachute system having a specified configuration. It was found (1) that the nonlinear elastic characteristics of the suspension system produce an amplification of the opening load when the viscous damping is negligible, (2) that the load amplification is markedly reduced when the suspension-line viscous damping coefficient is increased, and (3) that the suspension-line viscous damping is an important parameter of opening load amplification for high-velocity parachute inflations.
Document ID
19730034693
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Poole, L. R.
(NASA Langley Research Center Hampton, Va., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1973
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 10
Subject Category
Aircraft
Accession Number
73A19495
Distribution Limits
Public
Copyright
Other

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