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NASA NTRS ยท 19690037518

Structural and decelerator design options for Mars entry.

Abstract

Structural design options for decelerative aeroshell configurations for atmospheric entry on unmanned planetary explorations

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BibTeXRIS

Guy, L. D.. 1969-01-01. Structural and decelerator design options for Mars entry.. https://ntrs.nasa.gov/citations/19690037518

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