Corpus ID: 15008113

Development of Plasma Codes for the Design of Mini-Helicon Thrusters

@inproceedings{Pavarin2011DevelopmentOP,
  title={Development of Plasma Codes for the Design of Mini-Helicon Thrusters},
  author={D. Pavarin and Francesca Ferri and M. Manente and Davide Curreli and Davide Melazzi and D. Rondini and Alessandro Cardinali and Johan A. Carlsson},
  year={2011}
}
A compact low-power plasma thruster using high-efficiency radiofrequency sources is currently under development by the European consortium HPH.com “Helicon plasma hydrazine combined micro” (7th Framework Programme of European Union). The main objective of the HPH.com research is to design, optimize and develop a spacecraft thruster based on radiofrequency plasma source working in the helicon range, and investigate on applications to mini-satellites for attitude and position control. The design… Expand

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References

SHOWING 1-10 OF 11 REFERENCES
Feasibility Study of Medium-Power Helicon Thruster
A medium-power (1.5 kW) plasma thruster based on a helicon source is considered as a candidate for primary space propulsion. A high-density plasma is produced by the use of a radio frequency (RF)Expand
Helicon plasma hydra-zine : combined micro project overview and development status
TLDR
The objective of this research is to significantly improve knowledge on helicon-based plasma thrusters through deep numerical/theoretical investigations and extensive experimental campaigns, and then to apply the results to the design, optimization and development of a space plasma thruster. Expand
EXPERIMENTAL SET-UP TO TEST A 50 W HELICON PLASMA THRUSTER
This paper describes the experimental layout under development to test a helicon plasma thruster for a small satellite. The thruster class is 50 W 1mN. This work is done within the research projectExpand
Minihelicon Plasma Thruster
  • O. Batishchev
  • Materials Science
  • IEEE Transactions on Plasma Science
  • 2009
A compact high-power-density helicon plasma source operating on abundant medium atomic weight gases is under examination for a potential electric propulsion application. A high specific impulse,Expand
Equilibrium theory of cylindrical discharges with special application to helicons
Radiofrequency discharges used in industry often have centrally peaked plasma density profiles n(r) although ionization is localized at the edge, even in the presence of a dc magnetic field. This canExpand
VORPAL: a versatile plasma simulation code
VORPAL is a new plasma simulation code designed for maximum flexibility through use of advance C++ techniques. Through use of inheritance. VORPAL incorporates multiple models for the plasma andExpand
A Monte Carlo collision model for the particle-in-cell method: applications to argon and oxygen discharges
Abstract In order to use particle-in-cell (PIC) simulation codes for modeling collisional plasmas and self-sustained discharges, it is necessary to add interactions between charged and neutralExpand
An object-oriented electromagnetic PIC code
TLDR
The resulting code architecture, OOPIC (object-oriented particle-in-cell), is a two-dimensional relativistic electromagnetic PIC code that encapsulates key PIC algorithms and data into objects, simplifying extensions such as new boundary conditions and field algorithms. Expand
The 32 nd International Electric Propulsion Conference
  • The 32 nd International Electric Propulsion Conference
  • 2011
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