Thermodynamic Estimate of the Optimal Ratio of the Solid Propellant and Fuel in the Gas Generator of a High-Velocity Flying Vehicle
Crossref DOI link: https://doi.org/10.1134/S001050821906011X
Published Online: 2019-12-27
Published Print: 2019-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Salgansky, E. A.
Makhmudov, Kh. R.
Baikov, A. V.
Yanovskii, L. S.
Text and Data Mining valid from 2019-11-01
Version of Record valid from 2019-11-01
Article History
Received: 6 June 2018
Revised: 10 September 2018
Accepted: 12 September 2018
First Online: 27 December 2019