NASA NTRS · 19700016167
Apollo lunar module descent engine ablative chamber - Injector compatibility improvement study Summary report
Abstract
Summary of material and design improvements to reduce ablative chamber throat erosion in lunar module descent engine
Keep this discovery
Explore connections, maps & timelines
Maucieri, J. J.. 1969-12-24. Apollo lunar module descent engine ablative chamber - Injector compatibility improvement study Summary report. https://ntrs.nasa.gov/citations/19700016167
Cite the original work for its findings. Save a collection to share your selection of sources.