Research on Ablation Device Suitable for Thermal Protection System of Solid Rocket Ramjet

In solid rocket propulsion systems, overload effects induced by aircraft maneuvers can lead to gas accumulation in the afterburning chamber, resulting in severe localized ablation of thermal insulation layers and significantly compromising overall operational stability. Traditional ablation experime...

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发表在:	Aerospace
Main Authors:	Jiming Cheng, Hang Yan, Xiping Feng, Guoqiang Zhu, Jie Liu, Xintong Qi
格式:	文件
语言:	英语
出版:	MDPI AG 2025-08-01
主题:	solid rocket ramjet thermal protection system (TPS) ablation experimental device
在线阅读:	https://www.mdpi.com/2226-4310/12/9/772