|
LOW BURNING RATE COMPOSITE SOLID PROPELLANTS
Bajlovski Miomir Rodić Vesna Uzelac Mirko
The formulations of composite solid propellants with low burning rate hace been treated, The study has presented the effects of the solid phase content and formulation as well as the content of the burning rate depressor and the ammonium-perchlorate fraction ratio on the pressure exponent and rate in the burning rate law. The values of tensile strength and elongation at maximum force have been monitored as well.
Ključne reči: composite solid propellant, burning rate law, pressure exponent of burning rate, depressor, tensile stregth, elongation. |