NASA STI Repository (National Aeronautics and Space Administration) · 16 citations · 6 references
Open access
EngineeringAerospace EngineeringAerospace MaterialsPropulsionSpacecraft DesignHall Effect ThrustersMission RequirementsPropulsion System IntegrationPropulsion SystemsSpace ExplorationSystems Engineering For SpacecraftMission Concept DevelopmentPropellant Production In SpacePropulsion System DesignSpacecraft Architecture DesignThruster Design
The use of iodine propellant for Hall thrusters has been studied and proposed by multiple organizations due to the potential mission benefits over xenon. In 2013, NASA Marshall Space Flight Center competitively selected a project for the maturation of an iodine flight operational feed system through the Technology Investment Program. Multiple partnerships and collaborations have allowed the team to expand the scope to include additional mission concept development and risk reduction to support a flight system demonstration, the iodine Satellite (iSAT). The iSAT project was initiated and is progressing towards a technology demonstration mission preliminary design review. The current status of the mission concept development and risk reduction efforts in support of this project is presented.
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Performance Evaluation of an Iodine-Vapor Hall Thruster
James Szabo, Bruce Pote, Surjeet Paintal et al. · Journal of Propulsion and Power · 2012 · 115 citations