Burning-rate response functions of nitramine-based propellants and HMX from microthermocouple data measurements

Author:

Zenin A. A.,Finjakov S. V.

Publisher

Springer Science and Business Media LLC

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference27 articles.

1. B. V. Novozhilov, “Theory of nonstationary burning of homogeneous propellants,”Fiz. Goreniya Vzryva,4, No. 4, 482–490 (1968).

2. B. V. Novozhilov,Solid-Propellant Nonstationary Combustion [in Russian], Nauka, Moscow (1973).

3. E. W. Price, “Experimental observations of combustion instability,” in: K. K. Kuo and M. Summerfield (eds),Progress in Astronautics and Aeronautics, Vol. 90:Fundamentals of Solid-Propellant Combustion, AIAA, New York (1984), pp. 733–790.

4. J. S. T’ien, “Theoretical analysis of combustion instability,”ibid.,in: pp. 791–8400.

5. F. E. C. Culick and V. Yang, “Prediction of the stability of nonsteady motions in solid-propellant rocket motor,” in: L. De Luca, E. W. Price, and M. Summerfield (eds.),Progress in Astronautics and Aeronautics, Vol. 143:Nonsteady Burning and Combustion Stability of Solid Propellants, AIAA, Washington (1992), pp. 719–780.

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