Calculated results for the transient heating and melting process of glass shields with various material properties at the stagnation point of a re-entering ICBM /
John D. Warmbrod.

Description

Main Author

Warmbrod, John D.

Related Names

George C. Marshall Space Flight Center.
United States. National Aeronautics and Space Administration.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration, 1963.

Subjects

Protective coating.
Aerodynamic heating.
Space vehicles > Space vehicles / Atmospheric entry.

Physical Description

vii, 22 p. : ill. ; 27 cm.

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