Numerical and experimental investigation of throttleable hybrid rocket motor with aerospike nozzle
Hui Tian, Zihao Guo, Hao Zhu, Liu Hedong, Chengen Li
Topics & Concepts
NozzleSpecific impulseDischarge coefficientRocket engineThrustAerospace engineeringMass flow rateMechanical engineeringMechanicsSolid-fuel rocketRocket engine nozzleMass flowPropellantChemistryEngineeringPhysicsRocket and propulsion systems researchEnergetic Materials and CombustionSpace Exploration and Technology