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Area of Science:

  • Aerospace Engineering
  • Plasma Physics
  • Materials Science

Background:

  • Ionic wind propulsion is gaining attention for atmospheric propulsion.
  • Existing devices struggle to generate sufficient thrust for practical use.
  • Need for improved electrode designs to enhance thrust and efficiency.

Purpose of the Study:

  • To propose and evaluate a novel electrode structure for ionic wind propulsion.
  • To enhance ion generation and drift efficiency for increased thrust.
  • To develop a compact, lightweight, and structurally stable propulsion system.

Main Methods:

  • Designed a novel electrode structure featuring a serrated single-ring emitter and multi-ring collector.
  • Compared three electrode structures under varying voltages (20-40 kV), electrode gaps (60-120 mm), and ring diameters (60-100 mm).
  • Optimized structural parameters of the sawtooth multi-ring design.

Main Results:

  • The sawtooth multi-ring structure achieved a maximum thrust of 164 mN/m at 40 kV and a 60 mm gap.
  • Demonstrated a 1-2 times thrust increase due to enhanced ion generation and drift efficiency.
  • Achieved a 28.2% enhancement in thrust density through structural parameter optimization.

Conclusions:

  • The novel sawtooth multi-ring electrode structure significantly improves ionic wind propulsion performance.
  • The compact and lightweight design (17 g) offers practical advantages.
  • Results highlight the potential for low-altitude flight applications, with further optimization promising greater efficiency.