Investigation on combustion property of accelerated-aging CMDB solid propellant

Yunjun Luo; Xiaohu Yan; Huimin Tan; Wulin Qiu; Shanguo Luo

Investigation on combustion property of accelerated-aging CMDB solid propellant

Yunjun Luo
, Xiaohu Yan
, Huimin Tan
, Wulin Qiu
, Shanguo Luo

材料学院

Beijing Institute of Technology
Nanjing University

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

RTR system was used to investigate the combustion property of accelerated-aging CMDB solid propellant. The results indicate that aging process has no significant effects on burning rate, but can cause configuration damage. Experiments show that when aging temperature is over 70 °C and duration is over 24 days, abnormal combustion is obvious. Other additional experiments show that the aging temperature of 60 °C and the duration of 90 days could be considered as failure criteria of such CMDB solid propellant.

源语言	英语
页（从-至）	96-99
页数	4
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	20
期	4
出版状态	已出版 - 1999

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引用此

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abstract = "RTR system was used to investigate the combustion property of accelerated-aging CMDB solid propellant. The results indicate that aging process has no significant effects on burning rate, but can cause configuration damage. Experiments show that when aging temperature is over 70 °C and duration is over 24 days, abnormal combustion is obvious. Other additional experiments show that the aging temperature of 60 °C and the duration of 90 days could be considered as failure criteria of such CMDB solid propellant.",

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AU - Qiu, Wulin

AU - Luo, Shanguo

PY - 1999

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N2 - RTR system was used to investigate the combustion property of accelerated-aging CMDB solid propellant. The results indicate that aging process has no significant effects on burning rate, but can cause configuration damage. Experiments show that when aging temperature is over 70 °C and duration is over 24 days, abnormal combustion is obvious. Other additional experiments show that the aging temperature of 60 °C and the duration of 90 days could be considered as failure criteria of such CMDB solid propellant.

AB - RTR system was used to investigate the combustion property of accelerated-aging CMDB solid propellant. The results indicate that aging process has no significant effects on burning rate, but can cause configuration damage. Experiments show that when aging temperature is over 70 °C and duration is over 24 days, abnormal combustion is obvious. Other additional experiments show that the aging temperature of 60 °C and the duration of 90 days could be considered as failure criteria of such CMDB solid propellant.

UR - https://www.scopus.com/pages/publications/0032586460

M3 - Article

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SN - 1001-4055

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JO - Tuijin Jishu/Journal of Propulsion Technology

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Investigation on combustion property of accelerated-aging CMDB solid propellant

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