#4409 Electric Rocket Second Stage Analysis
#4409 Electric Rocket Second Stage Analysis #4409 Consider a totally electrical or electromagnetic propulsion second stage rocket. Transitioning to a fully electrical or electromagnetic second stage moves rocket propulsion away from chemical thermodynamics and into the realm of high-exhaust velocity physics. While chemical rockets are limited by the energy contained in molecular bonds, electromagnetic systems are limited only by the power available to the spacecraft. Here is an analysis of the primary architectures, the engineering hurdles, and the "Ideal Final Result" (IFR) for such a system. 1. Candidate Architectures A. Hall Effect Thrusters (HETs) & Gridded Ion Engines Currently the most flight-proven electric propulsion. They use electric fields to accelerate ionized gas (typically Xenon or Krypton). Pros: Extreme efficiency (Specific Impulse, I_sp , of 1,500s to 3,000s+ compared to ~450s for hydrogen-oxygen). Cons: Extremely low thrust-to-weight ratio. As a seco...