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Thermal and Mechanical Investigation of a Preload Release Mechanism for a Space Probe under Laboratory Conditions

Freukes, Christoph and Ksenik, Eugen and Grimm, Christian (2013) Thermal and Mechanical Investigation of a Preload Release Mechanism for a Space Probe under Laboratory Conditions. Bachelor's, Hochschule Niederrhein.

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Abstract

Der Vorspannungsabbau-Mechanismus der Asteroidenlandeeinheit MASCOT soll auf seine Funktionalität untersucht werden. Dazu muss ein Teststand entwickelt werden. Zusätzlich soll der Mechanismus derart verändert werden, dass der Erfolg des Abbauvorganges während des Fluges überprüft werden kann.

Item URL in elib:https://elib.dlr.de/104843/
Document Type:Thesis (Bachelor's)
Title:Thermal and Mechanical Investigation of a Preload Release Mechanism for a Space Probe under Laboratory Conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Freukes, ChristophChristoph.Freukes (at) dlr.deUNSPECIFIED
Ksenik, EugenDLR-Bremen, eugen.ksenik (at) dlr.deUNSPECIFIED
Grimm, ChristianChristian.Grimm (at) dlr.deUNSPECIFIED
Date:22 April 2013
Journal or Publication Title:Hochschule Niederrhein, Krefeld
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:91
Status:Published
Keywords:Mascot, Asteroiden, Lander, Separation, Preload Release Mechanism
Institution:Hochschule Niederrhein
Department:Fachbereich Maschinenbau und Verfahrenstechnik
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Science and Exploration
DLR - Research area:Raumfahrt
DLR - Program:R EW - Erforschung des Weltraums
DLR - Research theme (Project):R - Project MASCOT (old)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Explorationssysteme
Deposited By: Grimm, Christian
Deposited On:02 Aug 2016 11:39
Last Modified:31 Jul 2019 20:02

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