Erscheint 6 Ausgaben pro Jahr
ISSN Druckformat: 2150-766X
ISSN Online: 2150-7678
Indexed in
INVESTIGATION OF FUEL-RICH BORON COMBUSTION IN A PRESSURIZED COMBUSTION BOMB
ABSTRAKT
Small pellets of two different fuel-rich boron propellants were burnt in a pressurized combustion bomb in order to investigate the combustion in ducted rocket primary combustion chambers. The pressure varied between 1 and 100 bar. The combustion products were chemically analyzed for boron, boron oxide, and boron carbide. The results were plotted versus pressure and compared with computed equilibrium compositions. The main conclusion is that considerable extent of boron conversion into reaction products is already taking place in the primary gas generator of a ducted rocket.
-
Glotov Oleg G., Method of Model Agglomerates and Its Application to Study the Combustion Mechanisms of Al, Al+B, and Ti Particles, in Innovative Energetic Materials: Properties, Combustion Performance and Application, 2020. Crossref