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Postflight simulation of parachute deployment dynamics of Viking qualification flight testsSimulation calculations of the Viking qualification flight tests are conducted by use of analytical models of the parachute deployment dynamics process. Results from the study indicate that good simulations of event times and trajectory are obtained. If the full-scale parachute drag coefficient is used, a good simulation of first opening load is obtained and the overall nature of the load history is calculated. For longitudinal motions, the two-degree-of-freedom models give good agreement with a six-degree-of-freedom model. It is believed that the analytical models used are tools which will aid in the analysis of future flight systems.
Document ID
19730022109
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Whitlock, C. H.
(NASA Langley Research Center Hampton, VA, United States)
Poole, L. R.
(NASA Langley Research Center Hampton, VA, United States)
Talay, T. A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-7415
L-9145
Report Number: NASA-TN-D-7415
Report Number: L-9145
Accession Number
73N30841
Funding Number(s)
PROJECT: RTOP 815-20-09-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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