NASA NTRS · 19690029405
Obtaining hypervelocity acceleration using propellant-lined launch tubes Progress report
Abstract
Strain gages, nitrocellulose effects, and mathematical models for hypervelocity launch tubes with propellant lining
Keep this discovery
Explore connections, maps & timelines
Rodenberger, C. A.. 1969-05-01. Obtaining hypervelocity acceleration using propellant-lined launch tubes Progress report. https://ntrs.nasa.gov/citations/19690029405
Cite the original work for its findings. Save a collection to share your selection of sources.