Search NASASearch

NASA NTRS · 20200004222

Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles

Abstract

The source did not provide an abstract. Follow the original record for more information.

Keep this discovery

BibTeXRIS

David E Glass. Ceramic Matrix Composite (CMC) Thermal Protection Systems (TPS) and Hot Structures for Hypersonic Vehicles. https://ntrs.nasa.gov/citations/20200004222

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

KEEP EXPLORING

Related reports