Fiscal Year	2007
Division	Graduate School of Engineering & Applied Science
Department	Mechanical & Aerospace Engineering
Investigator(s)	Brophy, Christopher M.
Sponsor	Air Force Research Laboratory (Air Force)
Summary	Determine the heat transfer properties associated with plume impingement during the ignition and launch sequence of a solid propellant rocket motor. The heat transfer will be correlated to plume composition and additional IR imaging diagnostics.
Keywords
Publications	Publications, theses (not shown) and data repositories will be added to the portal record when information is available in FAIRS and brought back to the portal
Data	Publications, theses (not shown) and data repositories will be added to the portal record when information is available in FAIRS and brought back to the portal