Integral-Rocket Dual-Combustion Ramjets: A New Propulsion Concept

1980/09/01 by F. S. Billig, P. J. Waltrup, R. D. Stockbridge · 7 citations
Engineering · Mathematics · #Rocket and propulsion systems research #Energetic Materials and Combustion #Gas Dynamics and Kinetic Theory

paper · doi:10.2514/3.57760

Abstract

Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.

Cited by

• Influence of extruded injector nozzle on fuel mixing and mass diffusion of multi fuel jets in the supersonic cross flow: computational study. [europepmc]
• Investigation of unswept ramp system with lobe shape nozzle for fuel mixing of hydrogen jet at a scramjet engine. [europepmc]
• Usage of double injector for efficient mixing of the fuel behind the ramp injector at supersonic combustion chamber. [europepmc]
• Usage of serpentine injector for hydrogen mixing at combustion chamber of scramjet engine via a computational study. [europepmc]
• Using internal air injection for fuel mixing enhancement of annular hydrogen jet behind an inclined strut in a supersonic combustor: computational study. [europepmc]
• Optimization strut-based fuel injection using multi-step hydrogen jets and air-assisted mixing in supersonic flow. [europepmc]
• A novel strut injector with lateral extruded nozzle for efficient hydrogen mixing in supersonic combustors. [europepmc]

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