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Test/Model Correlation for Mars Pathfinder Multi-Body System Drop TestsA multi-body dynamics computer model was used extensively for the Mars Pathfinder mission to simulate its innovative and uncoventional atmospheric entry, descent and landing approach. To verify the accuracy and validity of this model was vital to the success of this mission, two multi-body system drop tests were performed and augmented by an extensive model correlation effort.
Document ID
20210005072
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
Authors
Smith, K. S.
Tsang, S. K.
Peng, C. Y.
Date Acquired
February 3, 1997
Publication Date
February 3, 1997
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Mars
Pathfinder
drop
test
drop
test
Mars
Pathfinder
EDL
lander
separation

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