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Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept — ReaderExpo

Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept

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Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept

by M. M. Fazah

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Rocket firingPropellant combustionTest firingHydrogen fuelsInjectorsFiring (Igniting)Rocket enginesEngine testsFuel combustionGas-gas interactions

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An engineering approach to modelling rocket motor ignition

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Automated propulsion data screening demonstraton system

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Plume diagnostics of the RSRM static firings for the pressure perturbation studies

Jay K. Sambamurthi