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CALCULATED RESULTS FOR THE TRANSIENT HEATING AND MELTING PROCESS OF GLASS SHIELDS WITH VARIOUS MATERIAL PROPERTIES AT THE STAGNATION POINT OF A RE-ENTERING ICBMCalculated results for transient heating and melting of glass shield at stagnation point of reentering icbm
Document ID
19630005471
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Warmbrod, J. D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1963
Subject Category
Space Sciences
Report/Patent Number
NASA-TN-D-1643
Report Number: NASA-TN-D-1643
Accession Number
63N15347
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SHIELDING
TRANSIENT HEATING
GLASS
REENTRY VEHICLE
INTERCONTINENTAL BALLISTIC MISSILE /ICBM/
STAGNATION POINT
MELTING

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