Thermodynamic Estimate of the Optimal Ratio of the Solid...

Combustion, Explosion, and Shock Waves 2019 / 11 Vol. 55; Iss. 6

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

Salgansky, E. A., Makhmudov, Kh. R., Baikov, A. V., Yanovskii, L. S.
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Volume:
55
Journal:
Combustion, Explosion, and Shock Waves
DOI:
10.1134/S001050821906011X
Date:
November, 2019
File:
PDF, 160 KB
2019
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