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- W2465696064 abstract "Despite the prevalence of small satellites in recent years, the systems flown to date have very limited propulsion capability. SmallSats are typically secondary payloads and have significant constraints for volume, mass, and power in addition to limitations on the use of hazardous propellants or stored energy. These constraints limit the options for SmallSat maneuverability. NASA's Space Technology Mission Directorate approved the iodine Satellite flight project for a rapid demonstration of iodine Hall thruster technology in a 12U (cubesat units) configuration under the Small Spacecraft Technology Program. The mission is a partnership between NASA MSFC, NASA GRC, and Busek Co, Inc., with the Air Force supporting the propulsion technology maturation. The team is working towards the critical design review in the final design and fabrication phase of the project. The current design shows positive technical performance margins in all areas. The iSat project is planned for launch readiness in the spring of 2017." @default.
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- W2465696064 date "2016-07-22" @default.
- W2465696064 modified "2023-09-25" @default.
- W2465696064 title "The Iodine Satellite (iSat) Project Development through Critical Design Review (CDR)" @default.
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- W2465696064 doi "https://doi.org/10.2514/6.2016-4540" @default.
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