A novel technique for the continuous evaluation of a burning rate of solid rocket propellant by using IR thermography

作者：Swiderski W^*; Miszczak M; Panas A

来源：QIRT Journal, 2011, 8(1): 111-114.

• Solid rocket propellant
• burning rate

IR thermography is proposed for the evaluation of a burning rate of cylindrical cores made of solid homogeneous propellants.

• 出版日期2011-6
• 单位中国人民解放军空军电子技术研究所