Dettleff, G. (2004) Plume Characterisation Testing of European Thrusters, Executive Summary. DLR-Interner Bericht. 224-2004 A 03, 103 S.
Full text not available from this repository.
An extensive study with 6 various subjects (work packages) has been performed to demonstrate the full plume test capacity available at DLR-Göttingen. This meant especially the use of the high vacuum facility STG with its helium-driven cryopump. In addition it could be shown how this facility and the Contamination Chamber CCG, where moderate vacuum can be achieved, complement one another. The study comprised 4 work packages with experimental work including investigations of the backflow and demonstration of the facilitys capacity to maintain space-like vacuum (<10-5 mbar) even when a 10N thruster is fired. The 2 other work packages dealt with possible future applications of STG: investigation of scaled thruster plumes and feasibility of electric thruster plume testing. On the whole 9 reports have been written to document the contract work.
|Document Type:||Monograph (DLR-Interner Bericht)|
|Title:||Plume Characterisation Testing of European Thrusters, Executive Summary|
|Number of Pages:||103|
|Keywords:||Thruster plume testing capacity, DLR high vacuum plume test facility STG, backflow|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||other|
|HGF - Program Themes:||other|
|DLR - Research area:||Space|
|DLR - Program:||no assignment|
|DLR - Research theme (Project):||UNSPECIFIED|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology|
|Deposited By:||Dagmar Brennecke-Hosseinzadeh|
|Deposited On:||31 Jan 2006|
|Last Modified:||14 Jan 2010 18:29|
Repository Staff Only: item control page