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DLR's Test Facility STG-ET

Neumann, Andreas (2013) DLR's Test Facility STG-ET. Trudy MAI (original: Труды МАИ), Vol. 60, pp. 1-8. Moskauer Staatliches Luftfahrt-Institut (nationale Forschungsuniversität).

Full text not available from this repository.

Official URL: http://www.mai.ru/science/trudy/

Abstract

Chemical and cold gas thruster plume flow and plume spacecraft interaction are subject of research and application at the German Aerospace Center, DLR, Germany, since about three decades. DLR is extending these activities in Göttingen to cover electric space propulsion testing and thruster investigation. For this purpose a new high vacuum facility, named STG-ET, has been built especially for electric propulsion testing. The vacuum chamber measures 12.2 m in length and 5 m in diameter. The design focus is on plume interaction with spacecraft components and on long-term tests. The facility will be equipped with advanced measurement methods for plasma analysis and thrust and thrust vector measurement. Inauguration of the facility took place in October 2011. This paper describes the facility, special design features, and first tests performed in the vacuum chamber.

Item URL in elib:https://elib.dlr.de/81233/
Document Type:Article
Title:DLR's Test Facility STG-ET
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Neumann, AndreasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2013
Journal or Publication Title:Trudy MAI (original: Труды МАИ)
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Vol. 60
Page Range:pp. 1-8
Publisher:Moskauer Staatliches Luftfahrt-Institut (nationale Forschungsuniversität)
Status:Published
Keywords:vacuum chamber, electric space propulsion, xenon, thruster, cryopump
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: Brennecke-Hosseinzadeh, Dagmar
Deposited On:15 Apr 2013 11:44
Last Modified:30 May 2013 03:02

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