Engineering Papers⌕ Search

NASA NTRS · 19720012855

Titanium reinforced boron-polyimide composite

Abstract

Processing techniques for boron polyimide prepreg were developed whereby composites could be molded under vacuum bag pressure only. A post-cure cycle was developed which resulted in no loss in room temperature mechanical properties of the composite at any time during up to 16 hours at 650 F. A design utilizing laminated titanium foil was developed to achieve a smooth transition of load from the titanium attachment points into the boron-reinforced body of the structure. The box beam test article was subjected to combined bending and torsional loads while exposed to 650 F. Loads were applied incrementally until failure occurred at 83% design limit load.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Clark, G. A., Clayton, K. I.. 1969-06-27. Titanium reinforced boron-polyimide composite. https://ntrs.nasa.gov/citations/19720012855

Cite the original work for its findings. Save a collection to share your selection of sources.