Thermal oxidation and heterogeneous combustion of AlH3 and Al: A comparative study

Author:

Liu Jianzhong,Yuan Jifei,Li Heping,Pang Aimin,Xu Peihui,Tang Gen,Xu Xingxing

Funder

National Natural Science Foundation of China

Open Research Fund Program of Science and Technology on Aerospace Chemical Power Laboratory

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. Agglomerates, smoke oxide particles, and carbon inclusions in condensed combustion products of an aluminized GAP-based propellant;Ao;Acta Astronaut.,2016

2. Mechanism of the organic fluoride effect on the formation of agglomerates and condensed products in the combustion of aluminised solid propellants;Zhou;Combust. Theor. Model.,2019

3. Solid propulsion for space applications: an updated roadmap;Guery;Acta Astronaut.,2010

4. The rapid H 2 release from AlH 3 dehydrogenation forming porous layer in AlH 3/hydroxyl-terminated polybutadiene (HTPB) fuels during combustion;Chen;J. Hazard Mater.,2019

5. Fundamental study on mechanisms of thermal decomposition and oxidation of aluminum hydride;Feng;J. Phys. Chem. C,2019

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