FIELD: testing hybrid rocket engines.
SUBSTANCE: proposed device has housing accommodating barrier ozonizer and precipitation condenser installed in tandem along gaseous emission flow and incorporating, respectively, parallel plate electrodes of two types, that is, charging and precipitation ones, with electric field built up in plate-to-plate gaps. Charging plates are connected to ac current supply rated at voltage higher than breakdown value; they are provided with barriers made in the form of insulating coatings and discharge gap between adjacent plates for passing gas emissions and forming corona discharge. Precipitation plates are connected to dc current supply rated at voltage lower than breakdown value.
EFFECT: facilitated permeability of gas jet for oxygen, enhanced corona discharge power and aerosol particle removal capability.
3 cl, 3 dwg
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Authors
Dates
2005-01-27—Published
2003-04-30—Filed