Development of the Linear Gridless Ion Thruster

نویسندگان

  • Brian E. Beal
  • Alec D. Gallimore
چکیده

The design of the Linear Gridless Ion Thruster, or LGIT, is presented in detail. The LGIT is a hybrid thruster that combines an ionization stage similar to those normally found on gridded ion engines with the acceleration mechanism of a Hall effect thruster. This thruster also features a linear geometry, which simplifies the design of the magnetic circuit while making the LGIT particularly well suited to future work on clustering and, perhaps, thrust vectoring by varying the magnetic fields in the acceleration zone. Initial testing with the thruster operating in a single-stage, unoptimized mode resulted in a specific impulse of 1400 seconds and an anode efficiency of 12%. The low efficiency is believed to be due in large part to operating the thruster in a single-stage mode, rather than the two-stage mode for which it was designed, and to setting the acceleration stage magnets to less than half their design value.

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Performance of a Linear Hall Discharge with an Open Electron Drift

This paper presents a recent characterization of the thrust efficiency and specific impulse of a low power, linear-geometry (non-coaxial) Hall thruster with an open electron-drift current. The thruster was constructed with a boron-nitride insulating channel surrounded by a magnetic circuit served by four electromagnet coils, and was designed to operate in the 100-Watt power class. A survey of t...

متن کامل

Recent Results from Internal and Very-Near-Field Plasma Diagnostics of a High Specific Impulse Hall Thruster

Floating potential and ion current density measurements were taken on the laboratory model NASA-173Mv2 in order to improve understanding of the physical processes affecting Hall thruster performance at high specific impulse. Floating potential was measured on discharge chamber centerline over axial positions spanning 10 mm from the anode to 100 mm downstream of the exit plane. Ion current densi...

متن کامل

Ion Thruster Development Trends and Status in the United States

The current interest in ion thrusters for near-Earth and deep-space missions has occurred because of long-term development efforts yielding an understanding of the physical phenomena involved in thruster operation and hardware that is suited to a wide range of missions. Features of state-of-the-art thrusters are described in terms of the various physical processes that occur within them. Tradeo...

متن کامل

Low Power Planar Antenna Inductive Discharge Ion Source

A 10 cm stand-alone gridded ion thruster discharge chamber based on a laboratory demonstration model that utilized a planar inductive antenna was designed and fabricated. The source features multipole confinement which has been shown to dramatically improve performance based on significant increases in ion density observed in demonstration tests. The thruster design considerations and the perfo...

متن کامل

The Effects of Clustering Multiple Hall Thrusters on Plasma Plume Properties

Clusters of Hall thrusters have been proposed as a means of achieving electric propulsion systems capable of operating at very high power levels. To facilitate testing in existing vacuum facilities, initial tests have focused on a cluster of low-power Busek BHT-200-X3 Hall thrusters. A combination of triple Langmuir probes and floating emissive probes is used to study the effects of multi-thrus...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2001