NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Convective and radiative heat transfer to an ablating body.Convective and radiative heat transfer to reentry vehicles protected by ablation heat shields
Document ID
19680056307
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hoshizaki, H.
Lasher, L. E.
Date Acquired
August 4, 2013
Publication Date
August 1, 1968
Subject Category
Thermodynamics And Combustion
Accession Number
68A37279
Funding Number(s)
CONTRACT_GRANT: NAS7-386
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available