New Sizing Methodology and Efficiency Analysis of Satellite’s Electrical Power Subsystem
Development of a High-Reliability Vacuum Arc Thruster System
Ignition and Extinction Characteristics of Electrically Controlled Solid Propellants
Performance Analysis of a Thermoelectric Combined Power Cycle
Temperature Evolution of Spark Kernels at Subatmospheric Pressures
Plume Composition Measurements of a High-Emission-Density Electrospray Thruster
Considerations for Reducing Aviation’s with Aircraft Electric Propulsion
Method for Estimation of Electrical Wiring Interconnection Systems in Preliminary Aircraft Design
Coordinated Model Predictive Control of Aircraft Gas Turbine Engine and Power System
Embodied Energy Repurposing via Energy-Harvesting Electrodynamic Tethers
Microcooling Channel Effect on a Monopropellant Microelectromechanical System Thruster Performance
Optimal Inerter-Based Shock–Strut Configurations for Landing-Gear Touchdown Performance
Influence of the Rotor Configuration on the Electrostatic Charging of Helicopters
Determining Electrical Ignition Characteristics of a Gas Propulsion System
Global Stability of a System with State-Dependent Riccati Equation Controller