Controllable digital solid state cluster thrusters for rocket propulsion and gas generation
A thruster stack assembly and method for manufacturing the same is provided. The thruster stack assembly includes a plurality of grain elements having a common core region (e.g., a channel or passageway), where each grain element comprises a volume of electrically ignitable propellant. The thruster...
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Main Author | |
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Format | Patent |
Language | English |
Published |
14.06.2011
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Subjects | |
Online Access | Get full text |
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