NASA NTRS · 19720000600
Study of high altitude plume impingement
Abstract
Computer program has been developed as analytical tool to predict severity of effects of exhaust of rocket engines on adjacent spacecraft surfaces. Program computes forces, moments, pressures, and heating rates on surfaces immersed in or subjected to exhaust plume environments. Predictions will be useful in design of systems where such problems are anticipated.
Keep this discovery
Explore connections, maps & timelines
Wojciechowski, C. J., Penny, M. M., Prozan, R. J., Seymour, D., Greenwood, T. F.. 1972-10-01. Study of high altitude plume impingement. https://ntrs.nasa.gov/citations/19720000600
Cite the original work for its findings. Save a collection to share your selection of sources.