NASA NTRS · 19750010243
Space shuttle maneuvering engine reusable thrust chamber program. Task 11: High epsilon injector test report
Abstract
A subscale injector test program conducted with a ten-inch diameter like-doublet injector to determine performance and heat flux profiles vs chamber pressure and propellant mixture ratio, and to determine stability characteristics with various acoustic cavity configurations is described. Results are presented.
Keep this discovery
Explore connections, maps & timelines
Pauckert, R. P.. 1974-12-01. Space shuttle maneuvering engine reusable thrust chamber program. Task 11: High epsilon injector test report. https://ntrs.nasa.gov/citations/19750010243
Cite the original work for its findings. Save a collection to share your selection of sources.