NASA NTRS · 19840003146
Metal matrix composite structural panel construction
Abstract
Lightweight capped honeycomb stiffeners for use in fabricating metal or metal/matrix exterior structural panels on aerospace type vehicles and the process for fabricating same are disclosed. The stiffener stringers are formed in sheets, cut to the desired width and length and brazed in spaced relationship to a skin with the honeycomb material serving directly as the required lightweight stiffeners and not requiring separate metal encasement for the exposed honeycomb cells.
Keep this discovery
Explore connections, maps & timelines
Mcwithey, R. R., Royster, D. M., Bales, T. T.. 1983-10-25. Metal matrix composite structural panel construction. https://ntrs.nasa.gov/citations/19840003146
Cite the original work for its findings. Save a collection to share your selection of sources.