Determination of Soot Particle Density and Dimension in the LOX/Kerosene Engine Booster Exhaust from Remote Measurements of Radiation Intensity

Details Determination of Soot Particle Density and Dimension in the LOX/Kerosene Engine Booster Exhaust from Remote Measurements of Radiation Intensity Determination of Soot Particle Density and Dimension in the LOX/Kerosene Engine Booster Exhaust from Remote Measurements of Radiation Intensity

Oct 2004

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2004esasp.557e..39p&link_type=abstract

Proceedings of the 2nd International Conference on Green Propellants for Space Propulsion (ESA SP-557). 7-8 June 2004, Chia Lagu

Computer Science

Scientific paper

As a result of comparison of experimental data to the modelling data of
own radiation of Atlas-III booster plume and the sunlight scattered by
the plume the soot mass concentration and mean-surface radius of soot
particles were determined at the nozzle exit which appeared equal to
0.17 % and 92 nm accordingly.

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