NASA NTRS · 19670032372
A method for obtaining temperature profiles for solid propellant motor exhaust streams.
Abstract
Theoretical analysis of heat transfer in solid propellant rocket exhaust plumes by use of temperature probe located in plume environment
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Mcgee, R. S., Say, M. B.. 1966-10-01. A method for obtaining temperature profiles for solid propellant motor exhaust streams.. https://ntrs.nasa.gov/citations/19670032372
Cite the original work for its findings. Save a collection to share your selection of sources.