One-dimensional modelling of the nozzle cooling with cryogenic oxygen flowing through helical channels in a hybrid rocket
Giuseppe Gallo, Landon T. Kamps, Shota Hirai, Carmine Carmicino, Harunori Nagata
Topics & Concepts
NozzleScramjetRocket engineRocket (weapon)Liquid-propellant rocketHeat transferCoolantMechanicsRocket engine nozzleAerospace engineeringWork (physics)PropellantLiquid oxygenMechanical engineeringFlow (mathematics)Mass flow rateMaterials scienceEngineeringPhysicsCombustionOxygenChemistryCombustorOrganic chemistryQuantum mechanicsRocket and propulsion systems researchHeat transfer and supercritical fluidsNuclear reactor physics and engineering