NASA NTRS · 19690040376
Thrust transient prediction and control of solid rocket engines.
Abstract
Analytical model for thrust-time curve during ignition transient of solid propellant rocket engines, discussing flame spreading
Keep this discovery
Explore connections, maps & timelines
Macdonald, B. W., Most, W. J., Stang, P. L., Summerfield, M.. 1968-10-01. Thrust transient prediction and control of solid rocket engines.. https://ntrs.nasa.gov/citations/19690040376
Cite the original work for its findings. Save a collection to share your selection of sources.