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Water pressure and accelerations during landing of a dynamic model of the Apollo spacecraft with a deployed-heat-shield impact-attenuation systemImpact water pressures, accelerations, and landing dynamics of scale model Apollo command module with deployed heat shield impact attenuation system
Document ID
19680009353
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Stubbs, S. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1968
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-4275
Report Number: NASA-TN-D-4275
Accession Number
68N18822
Funding Number(s)
CONTRACT_GRANT: 124-08-04-06-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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