TY - GEN
T1 - On the electrodeless MPD thruster using a compact helicon plasma source
AU - Toki, Kyoichiro
AU - Shinohara, Shunjiro
AU - Tanikawa, Takao
AU - Hada, Tohru
AU - Funaki, Ikkho
AU - Tanaka, Yoshikazu
AU - Yamaguchi, Akihiro
AU - Shamrai, Kostiantyn P.
PY - 2008
Y1 - 2008
N2 - Helicon wave excitation is one of the promising RF plasma production methods. It produces high density plasma (∼1013 cm-3) that enables electromagnetic acceleration. We prepared the acceleration coil or 2 pairs of copper plates around the glass tube. These acceleration methods are called a repetitious coil current acceleration and a continuous "Lissajous" acceleration, respectively. When the repetitious coil acceleration was applied, the maximum plasma velocity of 3.6 km/s was 76% velocity increment compared with before acceleration with the absorbed plasma production + acceleration power of (400+180) W and the applied magnetic field strength of 1,450 gauss. As for the "Lissajous" acceleration, the plasma velocity was 2.2 km/s with the absorbed plasma production + acceleration power of (290+200) W. However it is suggested that these accelerations remain in the thermal acceleration regime judging from the electron temperature or density increase.
AB - Helicon wave excitation is one of the promising RF plasma production methods. It produces high density plasma (∼1013 cm-3) that enables electromagnetic acceleration. We prepared the acceleration coil or 2 pairs of copper plates around the glass tube. These acceleration methods are called a repetitious coil current acceleration and a continuous "Lissajous" acceleration, respectively. When the repetitious coil acceleration was applied, the maximum plasma velocity of 3.6 km/s was 76% velocity increment compared with before acceleration with the absorbed plasma production + acceleration power of (400+180) W and the applied magnetic field strength of 1,450 gauss. As for the "Lissajous" acceleration, the plasma velocity was 2.2 km/s with the absorbed plasma production + acceleration power of (290+200) W. However it is suggested that these accelerations remain in the thermal acceleration regime judging from the electron temperature or density increase.
UR - http://www.scopus.com/inward/record.url?scp=77957853349&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=77957853349&partnerID=8YFLogxK
U2 - 10.2514/6.2008-4729
DO - 10.2514/6.2008-4729
M3 - Conference contribution
AN - SCOPUS:77957853349
SN - 9781563479434
T3 - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
BT - 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
PB - American Institute of Aeronautics and Astronautics Inc.
ER -