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Summary of design considerations for airplane spin-recovery parachute systemsA compilation of design considerations applicable to spin-recovery parachute systems for military airplanes has been made so that the information will be readily available to persons responsible for the design of such systems. This information was obtained from a study of available documents and from discussions with persons in both government and industry experienced in parachute technology, full-scale and model spin testing, and related systems.
Document ID
19720019383
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Burk, S. M., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-6866
L-8219
Report Number: NASA-TN-D-6866
Report Number: L-8219
Accession Number
72N27033
Funding Number(s)
PROJECT: RTOP 136-62-02-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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