Propulsion research on the hybrid plume rocket
, 1989 F. Chang-Diaz, T. Yang
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Journal of Aerospace Technology and Management, 2013 http://dx.doi.org/10.5028/jatm.v5i3.242 The purpose of this article is to present a study on the technological development of propellants, which are used in solid and hybrid rocket motor, that have been employing hydroxyl-terminated polybutadiene (HTPB)
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