Studies on Modification of Formulations of Composite Solid Propellant for Dual Thrust Rocket Motor
Journal Title: Problemy Mechatroniki. Uzbrojenie, lotnictwo, inżynieria bezpieczeństwa - Year 2011, Vol 2, Issue 2
Abstract
This paper presents the results of investigations of modified composite solid propellant charges for the dual made rocket motor. The modification has been done by selection of composition of the heterogeneous solid propellant made on the base of ammonium perchlorate as an oxidizer and the binder on the base of liquid rubber PBAN. As a result of modifications it was obtained the composite solid rocket propellant of better energetic and ballistic properties in comparison with the reference composite propellant.
Authors and Affiliations
Bogdan FLORCZAK, Andrzej CHOLEWIAK
Keywords
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