Operational characteristics of a representative Hollow Cathode Electron Emitter (HCE) device with C12A7:e- emitter

Type of the data
datacite.resourceTypeGeneral

Dataset

Total size of the dataset
datacite.size

6389379

Author
dc.contributor.author

Berka, Elisabeth

Author
dc.contributor.author

Wulfkühler, Jan-Philipp

Author
dc.contributor.author

Tajmar, Martin

Upload date
dc.date.accessioned

2025-12-19T12:02:13Z

Publication date
dc.date.available

2025-12-19T12:02:13Z

Publication date
dc.date.issued

2025-12-19

Abstract of the dataset
dc.description.abstract

Ignition and operation testing of the hollow cathode electron emitter (HCE) designed at the Institute of Aerospace Engineering of TUD Dresden University of Technology for the E.T.PACK-Fly in-orbit demonstration (IOD) mission with a C12A7:e- electron emitter. Testing conducted in triode mode with different laboratory electronics (e.g., 100–300 µF), krypton gas, and variable operating parameters (i.e., emission current and mass flow rate).

Public reference to this page
dc.identifier.uri

https://opara.zih.tu-dresden.de/handle/123456789/1918

Public reference to this page
dc.identifier.uri

https://doi.org/10.25532/OPARA-1053

Publisher
dc.publisher

Technische Universität Dresden

Licence
dc.rights

Attribution-NonCommercial-NoDerivatives 4.0 Internationalen

URI of the licence text
dc.rights.uri

http://creativecommons.org/licenses/by-nc-nd/4.0/

Specification of the discipline(s)
dc.subject.classification

4::43::406::406-01

Specification of the discipline(s)
dc.subject.classification

4::43::405::405-03

Title of the dataset
dc.title

Operational characteristics of a representative Hollow Cathode Electron Emitter (HCE) device with C12A7:e- emitter

Project abstract
opara.project.description

E.T.PACK-Fly is an EIC Transition Project funded by the European Innovation Council with 2.5 M€. The team of the project includes Universidad Carlos III de Madrid (UC3M, Coordinator), the University of Padova, the Technical University of Dresden (TU Dresden), the Spanish company SENER Aeroespacial and the German start-up Rocket Factory Augsburg (RFA). The main goal of E.T.PACK-F is to prepare a Ready-to-Fly (TRL 8) deorbit device based on ElectroDynamic Tether (EDT) technology. Two partners of the E.T.PACK-F consortium, SENER Aeroespacial and RFA, has signed a Launch Service Agreement to make an in-orbit-demonstration of the deorbit device in 2025.

Funding Acknowledgement
opara.project.fundingAcknowledgement

This research was funded by the European Commission’s H2020-FET-OPEN Research and Innovation Program through the European Commission’s Horizon Europe EIC Transition Program through the E.T.PACK-F Project under Grant 101058166.

Public project website(s)
opara.project.publicReference

https://etpack.eu/e-t-pack-f/

Project title
opara.project.title

E.T.PACK-F

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