Testing and Modeling Fuel Regression Rate in a Miniature Hybrid Burner

Ballistic characterization of an extended group of innovative HTPB-based solid fuel formulations for hybrid rocket propulsion was performed in a lab-scale burner. An optical time-resolved technique was used to assess the quasisteady regression history of single perforation, cylindrical samples. The...

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Bibliographic Details
Main Authors: Luciano Fanton, Christian Paravan, Luigi T. De Luca
Format: Article
Language:English
Published: Wiley 2012-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2012/673838
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