О методе оценки интегральных характеристик концептуального ГЛА с интегрированной двигательной установкой


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On the method for estimating the integral characteristics of a generic scramjet with an integrated propulsion system

This paper describes the method for estimating the integral characteristics of a generic scramjet with an integrated pro-pulsion system. Calculations of the specific impulse and heat fluxes in the propulsion system for the X-43 and X-51 generic scramjets have been carried out. The results obtained are in good agreement with the estimates of other au-thors, as well as with the known graphs of the dependence of the specific impulse for various types of engines depending on the flight Mach number.

scramjet, specific impulse, combustion

DOI: http://doi.org/10.33257/PhChGD.24.1.1017


Том 24, выпуск 1, 2023 год



В работе изложена методика оценки интегральных характеристик концептуального ГЛА с интегрированной двигательной установкой. Проведены расчеты удельного импульса и тепловых потоков в двигательной установке для ГЛА X-43 и X-51. Полученные резуль-таты находятся в хорошем соответствии с оценками других авторов, а также с извест-ными графиками зависимости удельного импульса для различных типов двигателей в зависимости от числа Маха полета. и типа используемого топлива.

ГЛА, удельный импульс, горение

DOI: http://doi.org/10.33257/PhChGD.24.1.1017


Том 24, выпуск 1, 2023 год



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