Research on the Combustion Properties of Propellants with Low Content of Nano Metal Powders

Author:

Zhi Jiang,Shu-Fen Li,Feng-Qi Zhao,Zi-Ru Liu,Cui-Mei Yin,Yang Luo,Shang-Wen Li

Publisher

Wiley

Subject

General Chemical Engineering,General Chemistry

Reference34 articles.

1. , Activated Aluminum as a Stored Energy Source for Propellants, in K. K. Kuo, et al., (Eds.), Challenges In Propellants And Combustion 100 Years After Nobel, Begell House, New York, 1997, p. 636.

2. M. J. Chiaverini, K. K. Kuo, A. Peretz, G. C. Harting, Heat Flux and Internal Ballistic Characterization of a Hybrid Rocket Motor Analog, 33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Seattle, WA, July 6–9, 1997, AIAA 1997–3080.

3. M. M. Mench, C. L. Yeh, K. K. Kuo, Propellant Burning Rate Enhancement and Thermal Behavior of Ultra-Fine Aluminum Powders (Alex), 29th Int. Annual Conference of ICT, Karlsruhe, Germany, June 30–July 3, 1998, p. 30/1.

4. Comparison of Thermal Behavior of Regular and Ultra-fine Aluminum Powders (Alex) Made from Plasma Explosion Process

5. N. Kubota, Y. Yano, T. Kuwahara, Particulate Damping of Acoustic Instability in RDX/AP Composite Propellant Combustion, 18th AIAA/SAE/ASME Joint Propulsion Conference, Cleveland, Ohio, June 21–23, 1982, p. 82–1223.

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