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The Iodine Satellite (iSat) Project Development Towards Critical Design ReviewDespite 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.
Document ID
20150016506
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Dankanich, John W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Calvert, Derek
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kamhawi, Hani
(NASA Glenn Research Center Cleveland, OH, United States)
Hickman, Tyler
(NASA Glenn Research Center Cleveland, OH, United States)
Szabo, James
(Busek (J.) Co., Inc. Natick, MA, United States)
Byrne, Lawrence
(Busek (J.) Co., Inc. Natick, MA, United States)
Date Acquired
August 26, 2015
Publication Date
July 6, 2015
Subject Category
Lunar And Planetary Science And Exploration
Spacecraft Propulsion And Power
Spacecraft Design, Testing And Performance
Report/Patent Number
M15-4663
Distribution Limits
Public
Copyright
Public Use Permitted.
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