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Abstract:

This segment explores three alternative propulsion methods for spacecraft once they are in orbit, contrasting them with the chemical rockets primarily used for Earth launch. It first details electric propulsion, or ion rockets, which use electricity from solar panels to ionize a gas, expelling it at extremely high velocities for subtle but sustained thrust, making them ideal for in-orbit maneuvering despite being too weak for launch. Next, nuclear thermal rockets are introduced, utilizing nuclear fission to superheat a propellant, achieving significantly higher exhaust velocities than chemical rockets for much faster deep-space travel, though they carry unacceptable safety risks for use near Earth. Finally, solar sails are described as a propellant-free concept that harnesses the momentum of photons on large reflective sheets, providing a tiny but continuous push suitable for extremely long, slow voyages over decades or centuries. The discussion concludes by reiterating the dominance of chemical rockets for launch, the growing adoption of electric propulsion for orbital corrections, and the potential future roles of nuclear and solar sails for deep-space or ultra-long-duration missions.

Exploring Alternatives to Chemical Rockets for In-Orbit Propulsion

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