NASA NTRS · 19700027045
Apollo spacecraft engine specific impulse, part 2
Abstract
Specific impulse of LM ascent and descent engines and SM engine
Keep this discovery
Explore connections, maps & timelines
Cuffe, J. P. B.. 1968-10-28. Apollo spacecraft engine specific impulse, part 2. https://ntrs.nasa.gov/citations/19700027045
Cite the original work for its findings. Save a collection to share your selection of sources.