NASA Technical Memorandum TM X-1669
X-15A-2 Unpredicted aerodynamic heating on Mach 6.7 flight
due to shock wave impingement

Click the title above or the image below to load the complete document.
(The complete document is a fairly large pdf file)


Cover image is from the monochrome rendition in the pdf file; cover color is reconstructed by copying the paper color from a scan of a different NASA technical report. Some of the stamped notations on the original document's cover may be in red ink.

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