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Bridle Attachment for Aircraft Spin-Recovery ParachuteAntispin rolling moment produced by chute drag force. Parachute stowed prior to deployment. At deployment, bridle attachment produces antispin rolling moment. At recovery, parachute forces are in aircraft plane of symmetry. Attachment system reduces parachute diameter typically required for spin recovery of experimental aircraft during harzardous flight testing.
Document ID
19840000357
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
White, W. L.
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 4
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LAR-13076
Accession Number
84B10357
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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