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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Bibliographic Details
Main Author SAWKA WAYNE N
Format Patent
LanguageEnglish
Published 14.06.2011
Subjects
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