FIELD: ecology. SUBSTANCE: method includes thermal decomposition, oxidation and stage neutralization of reaction final products in high-velocity transonic flow of working gas with M number M≥ 1 at oxidizer-excess coefficient of α≅ 1.1. Device has combustion chamber of rocket engine and mixing supersonic jet devices. EFFECT: higher efficiency. 2 cl, 1 dwg
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Authors
Dates
1994-01-15—Published
1992-05-19—Filed