NASA NTRS · 19690010478
Thermochemical ablation of rocket nozzle insert materials Final report
Abstract
Resistance of rocket nozzle throat insert materials to corrosion and melting
Keep this discovery
Explore connections, maps & timelines
Clark, K. J., Inouye, L. M., Kendall, R. M., Rindal, R. A.. 1968-02-15. Thermochemical ablation of rocket nozzle insert materials Final report. https://ntrs.nasa.gov/citations/19690010478
Cite the original work for its findings. Save a collection to share your selection of sources.