Methodical problems of solid-propellant burning-rate measurements using microwaves-Reference-Cited by-同舟云学术

Methodical problems of solid-propellant burning-rate measurements using microwaves

Published:2000-01 Issue:1 Volume:36 Page:62-71
ISSN:0010-5082
Container-title:Combustion, Explosion, and Shock Waves
language:en
Short-container-title:Combust Explos Shock Waves

Author:

Zarko V. E.,Vdovin D. V.,Perov V. 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

Link

http://link.springer.com/content/pdf/10.1007/BF02701515.pdf

Reference21 articles.

1. V. E. Zarko and K. K. Kuo, “Critical review of methods for regression rate measurements of condensed phase systems,” in: K. K. Kuo and T. Parr (eds.)Nonintrusive Combustion Diagnostics, Begel House, New York (1994), pp. 600–623.

2. L. D. Strand, K. R. Magiawala, and R. P. McNamara, “Microwave measurement of solid-propeliant pressure-coupled response function,”J. Spacecraft,17, No. 6 (1980).

3. D. T. Foss, R. J. Roby, and W. F. O’Brien, “Development of dual-frequency microwave burn-rate measurement system for solid rocket propellant,”J. Propuls. Power,9, No. 4 (1993).

4. P. Venugopalan, K. A. Jose, K. G. Nair, et al. “Microwave method for locating inhomogeneities in cured rocket propellant samples,”NDT Int.,19, No. 6 (1986).

5. B. Koch, “Reflexion de micro-ondes par des phenomenes de detonation,”C. R. Acad. Sci. Paris.,236, 661–663 (1953).

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