NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
THERMAL PROTECTION FOR SPACECRAFT ENTERING AT ESCAPE VELOCITYThermal protection for spacecraft entering at escape velocity
Document ID
19620002502
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Brooks, W. A., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Swann, R. T.
(NASA Langley Research Center Hampton, VA, United States)
Wadlin, K. L.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 1, 2013
Publication Date
January 1, 1962
Subject Category
Aircraft
Accession Number
62N12502
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REENTRY
THERMAL PROTECTION
SPACECRAFT
ABLATION
ESCAPE VELOCITY
HEATING
Document Inquiry

Available Downloads

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