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The Effect of Suspension-Line Length on Viking Parachute Inflation LoadsAnalytical calculations have considered the effect on maximum load of increasing the suspension-line length on the Viking parachute. Results indicate that unfurling time is increased to 1.83 seconds from 1.45 seconds, and that maximum loads are increased approximately 5 percent with an uncertainty of -4 percent to +3 percent.
Document ID
20060026138
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)
Charles H Whitlock
(Langley Research Center Hampton, United States)
Date Acquired
August 23, 2013
Publication Date
September 2, 1971
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Design, Testing and Performance
Report/Patent Number
LF99-3808
NASA-LWP-985
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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