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A Monte Carlo analysis of the Viking lander dynamics at touchdownThe performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all results are presented in statistical form. The primary objectives of this analysis were as follows: (1) to determine the three sigma design values of maximum rigid body accelerations and the minimum clearance of the lander body during landing; (2) to determine the probability of an unstable landing; and (3) to determine the probability of the lander body striking a rock. Two configurations were analyzed with the only difference being in the ability of the primary landing gear struts to carry tension loads.
Document ID
19750023452
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Muraca, R. J.
(NASA Langley Research Center Hampton, VA, United States)
Campbell, J. W.
(NASA Langley Research Center Hampton, VA, United States)
King, C. A.
(LTV Aerospace Corp. Hampton, Va., United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1975
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-7959
L-9830
Report Number: NASA-TN-D-7959
Report Number: L-9830
Accession Number
75N31525
Funding Number(s)
PROJECT: RTOP 815-20-01-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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