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- Article name
- ANALYSIS OF THE CONCEPTION OF HYPERSONIC AEROJET ENGINE WITH SPIN DETONATION COMBUSTION OF FUEL AND JOINING OF GAS MASS FOR INCREASE THRUST
- Authors
- Bogdanov V. I., , bogdanov-vasiliy@yandex.ru, PJSC "UEC-Saturn", Rybinsk, Yaroslavl region, Russia
- Keywords
- SCRAMJET / spin detonation / pulsating process / joining of mass / efficiency of the flight
- Year
- 2018 Issue 4 Pages 12 - 17
- Code EDN
- Code DOI
- Abstract
- The analysis of the possibility of creating a supersonic combustion ramjet engine (SCRAMJET) with spin detonation combustion of fuel and joining of gas mass for increase thrust in the pulsating process, which provides a flight speed corresponding of Mach number 8-10 is performed.
- Text
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