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The 250mN Thrust Balance for the DLR Goettingen EP Test Facility

Neumann, Andreas and Sinske, Julian and Harmann, Hans-Peter (2013) The 250mN Thrust Balance for the DLR Goettingen EP Test Facility. 33rd International Electric Propulsion Conference (IEPC2013), 2013-10-06 - 2013-10-10, Washington DC, USA.

Full text not available from this repository.

Official URL: http://www.iepc2013.org/agenda

Abstract

The German Aerospace Center DLR brought into operation a test facility for electric space propulsion in Goettingen, Germany, called STG-ET. This facility has been especially designed for electric propulsion with a vacuum chamber that measures more than 12m in length and 5m in diameter. Besides thruster performance tests the focus is on plume interaction with spacecraft components and on long-term testing. Thrust measurement is a fundamental measurement method for propulsion engine qualification. Ion and Hall effect space thrusters usually produce thrust levels in the milli-Newton range, and thrust balances have to deal with these low values. For the thrust balance of the STG-ET we adopted a thrust balance design based on a counter-balanced, electromagnetic force compensated device. The measurable thrust range is 250mN, but the design can easily accommodate an upgrade to 1N. The maximum allowed thruster assembly mass is 40kg. Several innovative features are implemented in its design.

Item URL in elib:https://elib.dlr.de/82209/
Document Type:Conference or Workshop Item (Speech)
Title:The 250mN Thrust Balance for the DLR Goettingen EP Test Facility
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Neumann, AndreasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Sinske, JulianUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Harmann, Hans-PeterAST, Bremen, GermanyUNSPECIFIEDUNSPECIFIED
Date:2013
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-10
Series Name:Conference Proceedings online
Status:Published
Keywords:electric propulsion, test facility, DLR, thrust balance
Event Title:33rd International Electric Propulsion Conference (IEPC2013)
Event Location:Washington DC, USA
Event Type:international Conference
Event Start Date:6 October 2013
Event End Date:10 October 2013
Organizer:George Washington University
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Anlagen u. Messtechnik (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Neumann, Andreas
Deposited On:05 Nov 2013 13:56
Last Modified:24 Apr 2024 19:48

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