elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Contact | Deutsch
Fontsize: [-] Text [+]

Planar Micro Nozzles - CFD Model Demands for Thrust Optimization

Banuti, Daniel and Grabe, Martin and Hannemann, Klaus (2014) Planar Micro Nozzles - CFD Model Demands for Thrust Optimization. Space Propulsion 2014, 19. - 22. May 2014, Cologne, Germany.

Full text not available from this repository.

Official URL: http://www.propulsion2014.com

Abstract

Regarding current trends in the miniaturization of satellites, an appropriate propulsion system is sought. Within the EU project PRECISE, a system analysis has shown that a MEMS (micro-electro-mechanical system) monopropellant hydrazine thruster has the potential to deliver thrust and Isp on a level that cannot be matched by other microsystems (e.g. cold gas). While manufacturers and researchers are experienced in catalyst and MEMS design, there is to date no standard or state-of-the-art in the analysis and design of high Reynolds number, micro scale, planar nozzles. Therefore, we undertook a systematic study of the modeling demands for such flows. A first part concerns the thermochemical fluid representation in CFD. We show that a constant property perfect gas representation will misevaluate thruster performance, as changes in the isentropic exponent have major impact on the theoretical exhaust velocity. The error grows with the complexity of the exhaust molecules and is more pronounced for molecules such as ammonia NH3 which is present in hydrazine decomposition. Hence, it is also important to model the gas composition as detailed as possible. Heat loss in the combustion chamber is assessed, which is very pronounced in micro scale systems. It is shown that a thus reduced chamber temperature strongly affects engine efficiency and hence also needs to be incorporated into any serious analysis. Finally, geometrical simplifications in CFD are regarded. We demonstrate that planar nozzle flows are inherently three dimensional in nature; CFD analysis of a 2D configuration will yield grossly wrong results as it cannot capture the boundary layers growing from the top and bottom wall. This effect is a lot more pronounced than the boundary layers growing from the contoured nozzle walls. All four boundary layers interact, choking the nozzle flow until it almost resembles a fully developed pipe flow.

Item URL in elib:https://elib.dlr.de/89116/
Document Type:Conference or Workshop Item (Speech)
Additional Information:Paper-Nr. SP2014-2967647, Session 4
Title:Planar Micro Nozzles - CFD Model Demands for Thrust Optimization
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Banuti, Danieldaniel.banuti (at) dlr.deUNSPECIFIED
Grabe, Martinmartin.grabe (at) dlr.deUNSPECIFIED
Hannemann, Klausklaus.hannemann (at) dlr.deUNSPECIFIED
Date:2014
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-9
Series Name:Confereance Proceedings on CD-ROM
Status:Published
Keywords:MEMS, CFD, micro, nozzle
Event Title:Space Propulsion 2014
Event Location:Cologne, Germany
Event Type:international Conference
Event Dates:19. - 22. May 2014
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Numerische Verfahren und Simulation
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Micknaus, Ilka
Deposited On:28 Aug 2014 10:04
Last Modified:20 Oct 2014 13:57

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.