1–20 of 89 hits
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    Ion Current Distribution of ECR Microwave Discharge Neutralizer

    Ohmichi, Wataru / Kuninaka, Hitoshi | AIAA | 2012

    Deep space flight of Hayabusa asteroid explorer

    Kuninaka, Hitoshi / Kawaguchi, Jun'ichiro | SPIE | 2008

    Overview of Electric Propulsion Activities in Japan (Invited)

    Komurasaki, Kimiya / Kuninaka, Hitoshi | AIAA | 2007

    Characteristics of Ion–Ion Thruster Generating Continuously Positive and Negative Ion Beams

    Koda, Daiki / Kuninaka, Hitoshi / Tsukizaki, Ryudo | AIAA | 2019

    In-flight operation of the Hayabusa2 ion engine system on its way to rendezvous with asteroid 162173 Ryugu

    Nishiyama, Kazutaka / Hosoda, Satoshi / Tsukizaki, Ryudo et al. | Elsevier | 2019

    Low Power Micro Ion Engine Using Microwave Discharge

    Koizumi, Hiroyuki / Kuninaka, HItoshi | AIAA | 2008

    Development of 20cm Diameter Microwave Discharge Ion Engine System "m20"

    Kuninaka, Hitoshi / Nishiyama, Kazutaka | AIAA | 2003

    Spacecraft charging due to lack of neutralization on ion thrusters

    Kuninaka, Hitoshi / Molina-Morales, Pedro | Elsevier | 2003

    GENERATOR AND METHOD FOR USING SAME

    Free access
    SONE YOSHITSUGU / KUNINAKA HITOSHI / TAKASHIMA TAKESHI et al. | European Patent Office | 2022

    Powdered Propellant PPT with Automatic Feed System

    Saito, Takefumi / Koizumi, Hiroyuki / Kuninaka, Hitoshi | AIAA | 2009