Atmospheric electroaerodynamic thrusters with grid collectors
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View abstract on PubMed
Summary
This summary is machine-generated.Grid structures significantly enhance electroaerodynamic (EAD) thruster performance. An optimal grid design boosts thrust density and thrust-to-weight ratio without reducing propulsive efficiency.
Area Of Science
- Aerospace Engineering
- Fluid Dynamics
- Electrical Engineering
Background
- Electaerodynamic (EAD) thrusters offer unique propulsion capabilities.
- Collector electrode design is crucial for optimizing EAD thruster performance.
- Existing literature lacks comprehensive studies on grid structures in EAD thrusters.
Purpose Of The Study
- To investigate the impact of grid collector electrode geometry on EAD thruster performance.
- To identify optimal grid parameters for enhanced thrust and efficiency.
- To compare performance with existing state-of-the-art EAD thrusters.
Main Methods
- Systematic experimental investigation of EAD thrusters with varying grid structures.
- Analysis of key geometric parameters: spatial density and wire diameter.
- Introduction of dimensionless coefficients for performance comparison.
Main Results
- An optimal grid configuration was identified, significantly improving performance.
- Maximum thrust density achieved was [Formula: see text] at [Formula: see text] applied voltage.
- Maximum thrust-to-weight ratio reached 9.51, maintaining propulsive efficiency.
Conclusions
- Grid structures are highly effective for enhancing EAD thruster performance.
- Optimized grid geometry offers a pathway to superior thrust density and thrust-to-weight ratios.
- The findings provide a foundation for designing next-generation EAD propulsion systems.
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