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The Effects of Parachute System Mass and Suspension-Line Elastic Properties on the LADT #3 Viking Parachute Inflation LoadAnalytical calculations have considered the effects of 1) varying parachute system mass, 2) suspension-line damping, and 3) alternate suspension-line force-elongation data on the canopy force history. Results indicate the canopy force on the LADT #3 parachute did not substantially exceed the recorded vehicle force reading and that the above factors can have significant effects on the canopy force history.
Document ID
20060026141
Acquisition Source
Langley Research Center
Document Type
Other - Working Papers
Authors
Theodore A Talay
(Langley Research Center Hampton, United States)
Lamont R Poole
(Langley Research Center Hampton, United States)
Date Acquired
August 23, 2013
Publication Date
December 30, 1971
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
LF99-3829
NASA-LWP-1021
Funding Number(s)
WBS: 857464.02.07.07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Langley Working Papers
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