Abstract
A systemic set of methods and devices designed to increase the maximum range of flight is considered. The main attention is paid to evaluation of efficiency for new technical solutions related to integrating the ramjet rocket engines into rocket vehicles with active and reactive launch principles. According to the results of studies, comparative assessments are presented for attainable values of the range increase based on the technical solutions considered.
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Original Russian Text © V.V. Vetrov, A.I. Diksheev, V.A. Dunaev, E.M. Kostyanoi, V.V. Morozov, 2015, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2015, No. 2, pp. 23–28.
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Vetrov, V.V., Diksheev, A.I., Dunaev, V.A. et al. On the concept of improving the ballistic efficiency of a rocket vehicle with the dominant midcourse phase. Russ. Aeronaut. 58, 160–166 (2015). https://doi.org/10.3103/S106879981502004X
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DOI: https://doi.org/10.3103/S106879981502004X