Fiscal Year	2010
Division	Graduate School of Engineering & Applied Science
Department	Mechanical & Aerospace Engineering
Investigator(s)	Brophy, Christopher M.
Sponsor	ATK Launch Systems (Other)
Summary	The Propellant Condensed Phase Characterization work will continue by directly imaging particle behavior inside a two-dimensional slab burner. The objective of this work is to directly image the aluminum oxide formation and behavior as the combustion products flow through a narrow passage between two propellant samples. NPS will test data and deliver a representative video documentation.
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