To achieve a rapid ionization rate of 1 kg/sec, significant power is required, estimated between 800 MW and 1.3 MW, depending on the material and efficiency. Current ion thruster designs are limited by power availability, and scaling them up would necessitate multiple engines and a substantial power source, likely nuclear. The feasibility of using pre-ionized fuel is questioned, as the energy required to store and accelerate such a large charge is immense and impractical. Chemical rockets remain more efficient for thrust compared to ionization methods, which face challenges in energy density and efficiency. Overall, while the concept of high-rate ionization is intriguing, the practical limitations make it a complex engineering challenge.