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Selectable-Towline Spin-Chute SystemSelectable-towline spin-chute system designed to enable in-flight deployment of single emergency spin-recovery parachute from more than one attachment point on airplane. Eliminates multiple parachutes and multiple deployment systems, reducing weight and cost of emergency system. Minimizes inertial and aerodynamic deviations on airplane, contributing to overall simplification of structure and aerodynamics.
Document ID
19910000606
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Vairo, Daniel M. (Planning Research Corp.)
Whipple, Raymond D. (NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 14, 2013
Publication Date
November 1, 1991
Publication Information
Publication: NASA Tech Briefs
Volume: 15
Issue: 11
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
LAR-14322
ISSN: 0145-319X
Report Number: LAR-14322
Accession Number
91B10606
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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