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VIBRATION TESTING OF THE Eu:CROPIS SATELLITE TEST STRUCTURE

Mierheim, Olaf und Glaser, Thilo und Hühne, Christian und Kottmeier, Sebastian und Hobbie, Catherin Fiona (2016) VIBRATION TESTING OF THE Eu:CROPIS SATELLITE TEST STRUCTURE. In: EUROPEAN CONFERENCE ON SPACECRAFT STRUCTURES, MATERIALS AND MECHANICAL TESTING, PROCEEDINGS. European Conference on Spacecraft Strucutres, Materials and Environmental Testing, 2016-09-27 - 2016-09-30, Toulouse, Frankreich.

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Kurzfassung

In the DLR (German Aerospace Center) compact satellite program the life supporting experiment Eu:CROPIS is developed. It is a small satellite weighing slightly more than 200kg. The proposed launch option is the Falcon 9 using the CASA adapter where it is placed on a balcony like support structure. The Eu:CROPIS satellite is being designed, produced and tested by DLR. Structural test for qualification are static and random loads, the random loads being the most demanding test. The static loads are tested using a sine burst test. As the structural test model is a prototype and as the project does not provide much time to repeat tests, the test sequence has been carefully chosen so as to limit structural damages before the end of the test campaign. Thus as many tests as possible are performed before the most demanding tests. Loads, stresses and deformations have been simulated by FEM-analyses before the tests. Still there are some uncertainties in the simulation due to the predicted damping and due to assumptions made to reduce the size and complexity of the model. Especially the random loads transfer into structural strain responses is very sensitive to the dynamic behavior. Therefore it is of interest to compare the assumed finite element structural response to the real measured one. For this purpose the test structure has been equipped with strain gauges to measure the peak strains in the primary structural parts in addition to the usual acceleration sensors. In this paper the test philosophy is explained using the prediction of structural stresses to sort the tests by intensity and thus by potential damage done to the tested structure. The measured natural frequencies, acceleration loads and internal strains are compared to the predicted ones. Reasons for deviations are given. The last test run showed significant changes in some acceleration responses. The search for the cause by analyses of the different acceleration responses is described.

elib-URL des Eintrags:https://elib.dlr.de/111597/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:VIBRATION TESTING OF THE Eu:CROPIS SATELLITE TEST STRUCTURE
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Mierheim, Olafolaf.mierheim (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Glaser, Thilothilo.glaser (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Hühne, Christianchristian.huehne (at) dlr.dehttps://orcid.org/0000-0002-2218-1223NICHT SPEZIFIZIERT
Kottmeier, SebastianSebastian.kottmeier (at) dlr.dehttps://orcid.org/0000-0001-8129-1644NICHT SPEZIFIZIERT
Hobbie, Catherin FionaCatherin.Hobbie (at) dlr.dehttps://orcid.org/0000-0002-3612-2785NICHT SPEZIFIZIERT
Datum:September 2016
Erschienen in:EUROPEAN CONFERENCE ON SPACECRAFT STRUCTURES, MATERIALS AND MECHANICAL TESTING, PROCEEDINGS
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Ja
Status:veröffentlicht
Stichwörter:Vibration Testing Shaker Random Sine Burst
Veranstaltungstitel:European Conference on Spacecraft Strucutres, Materials and Environmental Testing
Veranstaltungsort:Toulouse, Frankreich
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:27 September 2016
Veranstaltungsende:30 September 2016
Veranstalter :Cnes
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Forschung unter Weltraumbedingungen
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R FR - Forschung unter Weltraumbedingungen
DLR - Teilgebiet (Projekt, Vorhaben):R - Projekt eu:cropis (alt)
Standort: Braunschweig
Institute & Einrichtungen:Institut für Faserverbundleichtbau und Adaptronik > Funktionsleichtbau
Institut für Raumfahrtsysteme
Institut für Raumfahrtsysteme > Qualitätsmanagement
Hinterlegt von: Mierheim, Olaf
Hinterlegt am:29 Mär 2017 13:11
Letzte Änderung:24 Apr 2024 20:16

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