Combustion of Aluminum Particles near Burning Surface of Composite Propellant

Author:

TAKAHASHI Kenichi,NAKADAI Keita,TANABE Mitsuaki,KUWAHARA Takuo,SHIMADA Toru

Publisher

Japan Society for Aeronautical and Space Sciences

Reference11 articles.

1. 1) Guery, J.-F., Chang, I.-S., Shimada, T., Glick, M., Boury, D., Robert, E., Napior, J., Wardle, R., Pérut, C., Calabro, M., Glick, R., Habu, H., Sekino, N., Vigier, G. and d'Andrea, B.: Solid Propulsion for Space Applications: An Updated Roadmap, Acta Astronautica, 66 (2009), pp. 201-219.

2. 2) プロペラント専門部会: プロペラント.ハンドブック,(社)火薬学会,東京,2005, pp. 121-341.

3. 3) Kubota, N.: Propellants and Explosives, 2nd Edition, WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim, 2007, pp. 181-189.

4. 4) Takahashi, K., Mano, T., Tanabe, M., Kuwahara, T. and Shimada, T.: Velocity and Temperature Distributions around Metal Particles in the Reaction Zone of AP Composite Propellant, 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, AIAA Paper 2009-5428, 2009.

5. 5) Yang, V., Brill, T. B. and Ren, W.-Z.: Solid Propellant Chemistry, Combustion, and Motor Interior Ballistics, Progress in Astronautics and Aeronautics, Vol. 185, AIAA, VA, 2000, pp. 689-747.

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