Thermal performance of MMH/NTO rocket thrust chamber based on pintle injector by using liquid film cooling
Guodong Zhang, Guangxi Li, Longfei Li, G.H. Tang
Topics & Concepts
InjectorLiquid-propellant rocketPropellantCombustion chamberCoolantMaterials scienceThrustRocket engineChamber pressureMechanicsRocket (weapon)CombustionMechanical engineeringNuclear engineeringAerospace engineeringEngineeringChemistryPhysicsOrganic chemistryMetallurgyRocket and propulsion systems researchHeat transfer and supercritical fluidsEnergetic Materials and Combustion