Litcius/Paper detail

Optimum characteristic length of gas generator for liquid propellant rocket engine

Taj Wali Khan, Ihtzaz Qamar

2020Acta Astronautica20 citationsDOI

Topics & Concepts

Gas generatorPropellantInjectorLiquid-propellant rocketGenerator (circuit theory)Materials scienceVolumetric flow rateMechanicsRocket engineThrustMass flow rateMagnetohydrodynamic generatorSpecific impulseNuclear engineeringMechanical engineeringAerospace engineeringEngineeringThermodynamicsPhysicsPlasmaPower (physics)Quantum mechanicsMagnetohydrodynamicsRocket and propulsion systems researchHeat transfer and supercritical fluidsCombustion and Detonation Processes