Combustion Control of Solid Rocket Motors by Polytetrafluoroethylene Sublimates
Mass Flow Measurement Using Heat Transfer Method for Moved Bed Gravity Flow
Advantage of Using Oxygen as Plasma Jet Feedstock for Methane-Air Ignition
Homogeneous Charge Compression Ignition of Natural Gas-Air Mixture with Ozone Addition
Laser-Assisted Combustion of Solid Propellant at Low Pressures
Performance of Dimethyl Ether Arcjet Thrusters and Its Dependence on Electrode Configurations
Thrust Evaluation in Wide Frequency Range Using Active Control and Disturbance Observer