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

EAGLE: Cold Gas Thrusters Design and Tests

Dumont, Etienne and Dumke, Michael (2015) EAGLE: Cold Gas Thrusters Design and Tests. Other. DLR-Interner Bericht. SART TN-003/2015, 17 S. (Unpublished)

Full text not available from this repository.

Abstract

This report presents the design and test of the cold gas thrusters for the EAGLE vehicle Environment for Autonomous GNC Landing Experiments. First the theory of nozzle flow conditions is recalled. Then the evolution of the nozzle design during the design of the cold gas system is explained. Finally the test set-up is presented and the results analysed.

Item URL in elib:https://elib.dlr.de/103732/
Document Type:Monograph (DLR-Interner Bericht, Other)
Title:EAGLE: Cold Gas Thrusters Design and Tests
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Dumont, EtienneEtienne.Dumont (at) dlr.dehttps://orcid.org/0000-0003-4618-0572
Dumke, MichaelDLRUNSPECIFIED
Date:2015
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:17
Status:Unpublished
Keywords:EAGLE, RCS, nozzle, flow conditions
Institution:DLR: Institute of Space Systems
Department:Space Launcher Systems Analysis
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 - Systemanalyse Raumtransport
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Dumont, Etienne
Deposited On:05 Apr 2016 12:50
Last Modified:27 Oct 2016 11:10

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.