Workshop IPAIA2017 · sitael corresponding author: pduldqr dqguhqxffl#vlwdho frp 7kh lqfuhdvh ri dydlodeoh srzhu rq erdug ri prghuq vsdfhfudiw lv sdylqj wkh zd\ wr wkh xvh ri yhu\

$Page 1: Workshop IPAIA2017 · sitael corresponding author: pduldqr dqguhqxffl#vlwdho frp 7kh lqfuhdvh ri dydlodeoh srzhu rq erdug ri prghuq vsdfhfudiw lv sdylqj wkh zd\ wr wkh xvh ri yhu\$
International Workshop

IPAIA2017Ion Propulsion and Accelerator

Industrial Applications

CNR Research Area Bari Sala Congressi

March 1-3, 2017

International Scientific Advisory CommitteeE. Ahedo, UC3M, Madrid, SpainV. Antoni, CNR and Consorzio RFX, Padova, ItalyM. Cavenago (co Chair), INFN LNL Legnaro, ItalyR. Edgecock, STFC and Huddersfield University, UKS. Mazouffre, CNRS, Orleans, FranceF. Taccogna (co Chair), CNR Nanotec, Bari, ItalyV. Variale, INFN BA, Bari, Italy

Local Organizing CommitteeP. Minelli, CNR Nanotec, Bari, ItalyN. Ippolito, INFN BA, Bari, ItalyP. Veltri, INFN LNL and RFX Padova, Italy

SCOPE OF THE MEETING

This workshop will provide a forum for the presentation anddiscussion on the progress in methods and technologies used forthe research, development and industrial applications of ionpropulsion (IP) for satellite and spacecraft.

Special emphasis will be given to possible ion propulsionapplications to different technological fields such as energy(accelerator and ion sources for fusion) and material science (ionimplantation, surface treatment, nanoparticle synthesis).Subtopics include: Modelling and simulation, Progress made onthe different IP configurations, Plasma wall interaction, Ionsource physics, Accelerator Industrial Applications.

Venue is Area di Ricerca CNR di Bari, via Amendola 122/D, 70126Bari (Italy). For more information, see the Conference website:https://agenda.infn.it/conferenceDisplay.py?confId=12546

Sponsored by:

Application NetworkActivity Work Package 4

EUCARD2 Enhanced European Coordination for Accelerator Research &Development ,co funded from the European Commission under the FP7 Research Infrastructures GrantAgreement no. 312453

BOOK of ABSTRACT

International Workshop on Ion Propulsionand Accelerator Industrial Application

Wednesday 01 March 2017 - Friday 03 March 2017

CNR Nanotec, Bari, Italy

Book of abstracts

International Workshop on Ion Propulsion and Accelerator Industrial Application / Book ofabstracts

Friday 24 February 2017

i

Table of contents

High Power Hall Thruster Design at SITAEL ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1

Small rf plasma generator for air . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2

Carbon-based materials for cathode neutralizers in electric propulsion

Vibrational Kinetics of Electronically Excited States in H2 Discharges

.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

Electron drift instability and secondary electron emission in Hall effect thrusters: An insight frombidimensional particle-in-cell simulations .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

Helicon Propulsion Technology perspective for Minisatellites .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

ESA Perspectives on Electric Propulsion .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

Kinetic modeling of electrostatic ion thrusters

High thrust-over-power collisional Hall thruster

.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

Hybrid modelling of single and double stage hall thrusters .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

Experimental and theoretical study of ion beam neutralization by plasma ... . . . . . . . . . 11

Concepts in Low Power Hall Thruster Design - A Personal Perspective .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

Development of IPPLM's krypton HET ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

Ion Acceleration Mechanism in a Quad Confinement Thruster . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

Improvements in global modelling of gridded ion thrusters

A first review of facility effects on electric thruster testing

.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

.. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

The Hall thruster technology: from the classical design to the wall-less concept. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

Modeling magnetized plasma jets in electric propulsion .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

Hall Thruster numerical tool - Demo ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

Low Power Electric Propulsion Activities at Sitael . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

Development of Hollow Cathodes for Electric Thrusters: Theoretical and Experimental Results .. . . . . . . . . . . . . . . . . . 17

CIRA IMP-EP project: Development and validation of a 1D model for hollow cathode analysis and design .. . . 18

Hall thruster virtual lab .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

Hall Thrusters used as dissociator for fusion application .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

Wall interactions in Hall Effect Thruster, investigation with bidimensional Particle-in-cell model andsimulation .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . 20

Status of NIO1 negative ion source and acceleration system ... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

Modeling the electromagnetic field in anisotropic inhomogeneous magnetizedplasma of ecr ion sources .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

International Workshop on Ion Propulsion and Accelerator Industrial Application / Book of abstracts

1

22

High Power Hall Thruster Design at SITAEL

Sitael

Corresponding Author:


2

0

Small rf plasma generator for air

LNL

ITEP



3

21

Carbon-based materials for cathode neutralizers in electric propulsion

CNR-NANOTEC



4

10

Vibrational Kinetics of Electronically Excited States in H2 Discharges

Plasmi Lab at CNR-NANOTEC

CNR

Poliba



5

6

Electron drift instability and secondary electron emission in Hall effectthrusters: An insight from bidimensional particle-in-cell simulations

Laboratoire de Physique des Plasmas/Safran Aircraft EnginesLaboratoire de Physique des Plasmas/Centre National d'Etudes Spatiales

Laboratoire de Physique des Plasmas



6

19

Helicon Propulsion Technology perspective for Minisatellites

University of Padua

Technology for Propulsion and Innovation s.r.l

Università di Padova



7

16

ESA Perspectives on Electric Propulsion

European Space Agency

Europeans Space Agency



8

17

Kinetic modeling of electrostatic ion thrusters

Nuremberg Institute of Technology

University of Greifswald

University of Rostock



9

2

High thrust-over-power collisional Hall thruster

H.I.T. - Holon Institute of Technology



10

18

HYBRID MODELLING OF SINGLE AND DOUBLE STAGE HALLTHRUSTERS

Laplace, CNRS



11

27

EXPERIMENTAL AND THEORETICAL STUDY OF ION BEAMNEUTRALIZATION BY PLASMA

PPPL


5

Concepts in Low Power Hall Thruster Design - A Personal Perspective

Technion - Israel Institute of Technology



12

14

Development of IPPLM's krypton HET

Institute of Plasma Physics and Laser Microfusion

ESA-ESTEC



13

4

Ion Acceleration Mechanism in a Quad Confinement Thruster

Surrey Space CentreStanford Plasma Physics Laboratory



14

23

Improvements in global modelling of gridded ion thrusters

Laboratoire de physique des Plasmas

LPP, CNES

LPP


15

A first review of facility effects on electric thruster testing

LPP - UPMCLPP



15

7

The Hall thruster technology: from the classical design to the wall-lessconcept.

CNRS - ICARE

CorrespondingAuthor:

24

Modeling magnetized plasma jets in electric propulsion

Universidad Carlos III Madrid



16

28

Hall Thruster numerical tool - Demo

EnginSoftIMIP-CNR


12

Low Power Electric Propulsion Activities at Sitael

SITAEL



17

11

Development of Hollow Cathodes for Electric Thrusters: Theoretical andExperimental Results

Università di PisaSitael SpA



18

20

CIRA IMP-EP project: Development and validation of a 1D model forhollow cathode analysis and design

CIRA



19

25

Hall thruster virtual lab

CNR-Nanotec-PLasMICNR-Nanotec

ENGINSOFT


3

Hall Thrusters used as dissociator for fusion application

CNR-Nanotec-PLasMI



20

13

Wall interactions in Hall Effect Thruster, investigation withbidimensional Particle-in-cell model and simulation

LPPLaboratoire de Physique des Plasmas/Safran Aircraft Engines


9

Status of NIO1 negative ion source and acceleration system

LNLConsorzio RFX



21

8

MODELING THE ELECTROMAGNETIC FIELD IN ANISOTROPICINHOMOGENEOUS MAGNETIZED PLASMA OF ECR ION SOURCES

LNS

LNL

UniCT, LNS


Documents

Workshop IPAIA2017 · sitael corresponding author: pduldqr dqguhqxffl#vlwdho frp 7kh lqfuhdvh ri dydlodeoh srzhu rq erdug ri prghuq vsdfhfudiw lv sdylqj wkh zd\ wr wkh xvh ri yhu\