Thrust Evaluation in Wide Frequency Range Using Active Control and Disturbance Observer
Performance of Dimethyl Ether Arcjet Thrusters and Its Dependence on Electrode Configurations
Laser-Assisted Combustion of Solid Propellant at Low Pressures
Intense Tangential Pressure Oscillations Inside a Cylindrical Chamber
Homogeneous Charge Compression Ignition of Natural Gas-Air Mixture with Ozone Addition
Conceptual study and key technology development for Mars Aeroflyby sample collection
Combustion Control of Solid Rocket Motors by Polytetrafluoroethylene Sublimates