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System tests were performed in which Integrally Regulated Solar Arrays (IRSA's) were used to directly power the beam and accelerator loads of a 30-cm-diameter, electron bombardment, mercury ion thruster. The remaining thruster loads were supplied from conventional power-processing circuits. This combination of IRSA's and conventional circuits formed a hybrid power

Title : Operational Compatibility of 30-Centimeter-Diameter Ion Thruster with Integrally Regulated Solar Array Power Source
Author : National Aeronautics and Space Administration
Language : en
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Type : PDF, ePub, Kindle
Uploaded : Apr 07, 2021

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