The fitting of parameters of the hyperacoustic entering device and afterburning chamber of the rocket-based-combined-cycle engine
Heading:
| 1Katrenko, MA, 1Gorbenko, GA 1Oles Honchar National University of Dnipropetrovsk, Dnipropetrovsk, Ukraine |
| Kosm. nauka tehnol. 2003, 9 ;(Supplement1):139-142 |
| https://doi.org/10.15407/knit2003.01s.139 |
| Publication Language: Russian |
Abstract: 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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