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Performance evaluation of 'thermo-lag' material for entry heat protection of advanced manned spacecraft. vol. 1- summary of investigations final report, 1 oct. 1962 - 31 jan. 1964Thermoconductivity and thermal properties of protective coating and structural material for reentry manned spacecraft
Document ID
19650015245
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
August 2, 2013
Publication Date
February 28, 1964
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-65015
Report Number: NASA-CR-65015
Accession Number
65N24846
Funding Number(s)
CONTRACT_GRANT: NAS9-877
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STRUCTURAL MATERIAL
REENTRY VEHICLE
MANNED SPACECRAFT

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