The fitting of parameters of the hyperacoustic entering device and afterburning chamber of the rocket-based-combined-cycle engine

1Katrenko, MA, 1Gorbenko, GA
1Oles Honchar National University of Dnipropetrovsk, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 2003, 9 ;(Supplement1):139-142
Publication Language: Russian
We consider the basic approaches to definition of requirements of the joint operation of the hyperacoustic rotationally symmetric entering device and afterburning chamber of a missile stage of an ideal rockct-based-combined-cyclc engine.
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