A Rational Design Method for the Nagoya Type-III Antenna
The current study, as part of a PhD project on the design of a helicon thruster, aims to provide a rational methodology for the design of the helicon thruster’s main component, i.e., the helicon antenna. A helicon thruster is an innovative electrodeless plasma thruster that works by exciting helicon...
Saved in:
| Main Authors: | Daniele Iannarelli, Francesco Napoli, Antonella Ingenito, Alessandro Cardinali, Antonella De Ninno, Simone Mannori |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2024-12-01
|
| Series: | Aerospace |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2226-4310/11/12/1056 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
A study of an air-breathing electrodeless plasma thruster discharge
by: J. Zhou, et al.
Published: (2024-12-01) -
Development of the RF Ion Sources for Focused Ion Beam Accelerators
by: V. Voznyi, et al.
Published: (2014-01-01) -
Power absorption in the plasma ion source of a helicon type
by: S. N. Mordyk, et al.
Published: (2011-12-01) -
Numerical simulation of thermo-throttle for iodine flow rate control in multidirectional plasma thruster [version 1; peer review: 2 approved]
by: Pavel Savelev, et al.
Published: (2023-10-01) -
Numerical optimization of Hall effect thruster with variation in magnetic field
by: Harshit Shukla, et al.
Published: (2025-06-01)