Investigations on the thermal response of a solid rocket motor with complex charge structure using CL-20/GAP propellant

Investigations on the thermal response of a solid rocket motor with complex charge structure using CL-20/GAP propellant

The thermal safety of a solid rocket motor with a complex charge structure using CL-20 (Hexanitrohexaazaisowurtzitane)/GAP (Glycidyl Azide Polymer) propellant was evaluated. The morphology and thermal decomposition properties of the propellant were first studied by differential thermal analysis, the...

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Bibliographic Details
Main Authors: Yiyao Wang, Junjie Wen, Junsen Yang, Guanglong Zhang, Ningfei Wang, Yi Wu
Format: Article
Language:English
Published: Elsevier 2022-09-01
Series:Case Studies in Thermal Engineering
Subjects:
GAP/CL-20 propellant
Cook-off experiments
Thermal response of solid rocket motor
Complex motor charge structure
Online Access:http://www.sciencedirect.com/science/article/pii/S2214157X22005032

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http://www.sciencedirect.com/science/article/pii/S2214157X22005032

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