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An experimental comparison of three typical Mars entry body shapes on the basis of total equilibrium shock-layer radiationComparative study of total equilibrium shock layer radiation for three potential Mars entry body shapes
Document ID
19670008619
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dyner, H. B. (Avco Corp. Wilmington, MA, United States)
Reinecke, W. G. (Avco Corp. Wilmington, MA, United States)
Date Acquired
August 3, 2013
Publication Date
October 10, 1966
Subject Category
Thermodynamics And Combustion
Report/Patent Number
AVSSD-0228-66-RR
NASA-CR-81675
Report Number: AVSSD-0228-66-RR
Report Number: NASA-CR-81675
Accession Number
67N17948
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: JPL-951331
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MARS /PLANET/
SHOCK LAYER
RADIATIVE HEAT TRANSFER
REENTRY BODY

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