Thermodynamic Estimate of the Optimal Ratio of the Solid Propellant and Fuel in the Gas Generator of a High-Velocity Flying Vehicle-Reference-Cited by-同舟云学术

Thermodynamic Estimate of the Optimal Ratio of the Solid Propellant and Fuel in the Gas Generator of a High-Velocity Flying Vehicle

Published:2019-11 Issue:6 Volume:55 Page:702-707
ISSN:0010-5082
Container-title:Combustion, Explosion, and Shock Waves
language:en
Short-container-title:Combust Explos Shock Waves

Author:

Salgansky E. A.,Makhmudov Kh. R.,Baikov A. V.,Yanovskii L. S.

Publisher

Pleiades Publishing Ltd

Subject

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

Link

http://link.springer.com/content/pdf/10.1134/S001050821906011X.pdf

Reference14 articles.

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2. E. L. Kondratyuk, “Investigations performed in the USA in the Field of the Development of Hypersonic Flying Vehicles,” Dvigatel 85 (1), 8–11 (2013).

3. V. A. Shandakov, A. S. Zharkov, V. N. Strelnikov, et al., Physical and Chemical Fundamentals of Creation of Elements for Low-Temperature Gas Generators for Various Purposes (Fizmatlit, Moscow, 2011) [in Russian].

4. S. V. Kalinin, A. I. Shaburin, V. I. Sarab'ev, et al., “Investigation of Thermodynamic Characteristics of Pyrotechnical Gas-Generating Compositions for Low-Temperature Gas Generators,” Vestn. Tekhnol. Univ. 20 (2), 44–46 (2017).

5. K. Yu. Aref'ev, K. V. Fedotova, L. S. Yanovskii, et al., “Investigation of the System for Cooling Cylindrical Channels by Products of Gasification of Solid Hydrocarbon Fuels,” Izv. Vyssh. Uchebn. Zaved., Mashinostr., No. 1, 86–98 (2017).

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