Performance of a Pulsed Plasma Thruster Using Double Discharge Method
2002-01-0990: Development of the Toyota Mild-Hybrid System (THS-M)
Development of Toyota Mild Hybrid System (THS-M) with 42V PowerNet^1
Ultrafast intersubband relaxation at 1.55 mum in GaN/AlN MQWs
Developing Interior Material with Tactile Improvement
Advantage of Using Oxygen as Plasma Jet Feedstock for Methane-Air Ignition
Use of Solid Chemical Propellants for Coaxial Pulsed Plasma Thrusters
Homogeneous Charge Compression Ignition of Natural Gas-Air Mixture with Ozone Addition