، صفحه 0-0 (1)

عنوان دوره: اولین دوره بین المللی و بیست و هشتمین دوره ملی (1400)

A microwave electrothermal thruster has been constructed, consisting of a microwave plasma chamber 12cm long and 8cm in inner diameter and a micronozzle 10mm long with 1mm in diameter. The microwave plasma produced by 2.45GHz microwave frequency at power 1kW and the feed gas is Ar at pressure of 10^-3mTorr. The plasma density and electron temperature are and 2.1eV, respectively. The thrust and specific impulse are 10mN and 100s.

microwave plasma؛ electrothermal؛ thruster؛ spacecraft