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International Journal of Energetic Materials and Chemical Propulsion
ESCI SJR: 0.28 SNIP: 0.421 CiteScore™: 0.9

ISSN Imprimer: 2150-766X
ISSN En ligne: 2150-7678

International Journal of Energetic Materials and Chemical Propulsion

DOI: 10.1615/IntJEnergeticMaterialsChemProp.v5.i1-6.390
pages 366-374

PARAMETRIC INVESTIGATION OF SUPERSONIC COMBUSTION OF SOLID FUELS

Igor Feldman
Faculty of Aerospace Engineering, Technion - Israel Institute of Technology, Haifa 32000, Israel
Alon Gany
Sylvia and David IA Fine Rocket Propulsion Center and the Aerothermodynamics Lab, Faculty of Aerospace Engineering, Technion – Israel Institute of Technology, Haifa, 3200003, Israel

RÉSUMÉ

An experimental investigation of a solid fuel scramjet combustor was aimed at determining the combustion characteristics of different types of solid fuels. In particular, comparison was made between the results from a fuel-rich solid propellant (60% hydroxyl-terminated-polybutadiene HTPB and 40% ammonium perchlorate AP) vs. those of a polymethyl-methacrylate PMMA fuel. While born fuels exhibited a similar general behavior, the PMMA fuel showed a better flameholding capability, while the HTPB/AP fuel-rich propellant yielded a much higher regression rate.


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