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
Keep this discovery
Explore connections, maps & timelines
Guy, L. D.. 1969-01-01. Structural and decelerator design options for Mars entry.. https://ntrs.nasa.gov/citations/19690037518
Cite the original work for its findings. Save a collection to share your selection of sources.