Burning Rate Estimate Method of Solid Propellants at High Pressure Condition

Author:

Choi Hanyoung,Lee Dongsun,Sung Hong-Gye,Lee Wonmin,Kim Eunmi

Funder

Defense Industry Technology Center

Publisher

The Korean Society of Propulsion Engineers

Subject

General Medicine

Reference14 articles.

1. Cho, M.G., Heo, J.Y. and Sung, H.G., “Unsteady Internal Ballistic Analysis for Solid Rocket Motors with Erosive Burning,” Journal of the Korean Society of Propulsion Engineers, Vol. 13, No. 2, pp. 17-25, 2009.

2. Gupta, G., Jawale, L., Mehilal, D. and Bhattacharya, B., “Various Methods for the Determination of the Burning Rates of Solid Propellants – An Overview,” Central European Journal of Energetic Materials, Vol. 12, No. 3, pp. 593-620, 2015.

3. Direct Determination of Burning Rates of Propellant Powders

4. Measurement of solid propellant burning rates by analysis of ultrasonic full waveforms

5. An Optical System for Measuring the Burning Rate of Solid Propellant Strands

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Combustion Efficiency Estimation Method of Solid Propellants and the Effects of Grain Shape using Closed Bomb Test;Journal of the Korean Society of Propulsion Engineers;2022-12-31

2. CBT Combustion Precise Modeling and Analysis Using VOF and FSI Methods;Journal of the Korean Society of Propulsion Engineers;2022-10-31

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