This investigation continued the development of a method
for obtaining high quality holograms of the combustion
products from metallized solid rocket motor propellants
burned in a two-dimensional motor to provide a cross-flow
environment. The use of borosilicate side plates as a motor
casing allowed good quality holograms to be obtained. With
the present two-dimensional motor method there were upper
limits of combustion pressure and weight percentage of
aluminum where holograms could not be obtained because of
excessive smoke opacity.http://archive.org/details/holographicinves00leeyF04611-84-X-0001Major, Republic of Korea Air ForceApproved for public release; distribution is unlimited