5 South Zhongguancun street
Center for Energy and Environmental Policy Researc
Beijing, 100081
China
Beijing Institute of Technology
Solid fuel ramjets, Multi-ring diaphragm, Afterburning chamber, Combustion efficiency, Mixing and combustion
proton exchange membrane, water electrolytic cell, microgravity condition, heat transfer, mass transfer
Aluminum particles, Al-based metal alloy, Ignition delay time, Combustion characteristics, minimum ignition energy
Gravitational wave detection, Drag-free control, Micro-DC ion thruster, Thrust noise
Solid rocket ramjets, Inlet, Flow distortion, Combustion efficiency.