The Problem of Optimal Discharge Energy in an Ablative Pulsed Plasma Thruster
Development of an SPT-100VT Stationary Plasma Thruster with Increased Thrust
Development of an SPT-100VT Stationary Plasma Thruster with Increased Thrust
Electro-rocket ramjet thruster for compensating the aerodynamic drag of a low-orbit spacecraft
Electro-rocket ramjet thruster for compensating the aerodynamic drag of a low-orbit spacecraft
Electric Propulsions as Actuators of the Spacecraft Flight Control Systems
The Use of a Solar Electrojet Propulsion System for Jupiter Satellite Injection
The Use of a Solar Electrojet Propulsion System for Jupiter Satellite Injection
Project Analysis of Power and Mass Performance of Space Solar Arrays in the Wide Power Range