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Cited article:
A. Weinstein , A. Gany
Published online: 2013-03-05
This article has been cited by the following article(s):
13 articles
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Excessive Subsurface Heat Release As a Possible Cause of the Negative Erosion Effect during Combustion of Homogeneous Solid Propellants
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Numerical Analysis of Paraffin-Wax/Oxygen Hybrid Rocket Engines
Mario Tindaro Migliorino, Daniele Bianchi and Francesco Nasuti Journal of Propulsion and Power 36 (6) 806 (2020) https://doi.org/10.2514/1.B37914
Numerical simulation of low-melting temperature solid fuel regression in hybrid rocket engines
S.A. Rashkovskiy and S.E. Yakush Acta Astronautica 176 710 (2020) https://doi.org/10.1016/j.actaastro.2020.05.002
Enhancement of the Fuel Regression Rate in Hybrid Propulsion by Expandable Graphite Additive
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Kenneth L. Budzinski and Paul DesJardin (2020) https://doi.org/10.2514/6.2020-3749
Radiation heat transfer in ablating boundary layer combustion theory used for hybrid rocket motor analysis
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A review of the performance and structural considerations of paraffin wax hybrid rocket fuels with additives
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Study of Thermo-Mechanical Properties of HTPB–Paraffin Solid Fuel
Yogesh Kumar Sinha, B. T. N. Sridhar and R. Kishnakumar Arabian Journal for Science and Engineering 41 (11) 4683 (2016) https://doi.org/10.1007/s13369-016-2230-3