Updated conceptual design of hydrogen/ethylene fueled detonation ramjet: Test fires at Mach 1.5, 2.0, and 2.5
V. S. Ivanov, С. М. Фролов, А. Э. Зангиев, В. И. Звегинцев, И. О. Шамшин
Topics & Concepts
DetonationCombustorRamjetSpecific impulseMach numberEquivalence ratioAerospace engineeringHydrogenScramjetThrustAerodynamicsPropellantNuclear engineeringEngineeringMaterials scienceCombustionChemistryExplosive materialOrganic chemistryCombustion and Detonation ProcessesFire dynamics and safety researchRisk and Safety Analysis