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Development of the Support System Used on the HP3 Instrument for Insight Mars Mission

Reershemius, Siebo und Fittock, Mark und Spröwitz, Tom und Spohn, Tilman (2016) Development of the Support System Used on the HP3 Instrument for Insight Mars Mission. 14th European Conference on Spacecraft Structures, Materials and Environmental Testing, 2016-09-27 - 2016-09-30, Toulouse, France.

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Kurzfassung

An overview of the development and the qualification process of the Support System is presented. The relevant requirements, the mechanical design and the environmental testing are described. The mechanical design of the Support System is mainly driven by a new and unique set of requirements derived from the working environment on Mars, the autonomous mechanical operation on the surface and the deployment from the lander deck. The resulting relevant sub-system requirements are presented. Furthermore the instruments design is explained to show, which design elements have been implemented to ensure proper functionality. One major group of design elements, which is described in detail, are the various mechanisms. Details on the used actuators and their functionality are also presented. Various verification tests had to be performed in the course of HP3 Support System development. Besides the standard thermal-vacuum and vibration tests, special tests have been executed to show compliance of the instrument design to the requirements. These tests are: Separation Tests from the lander deck in cold environment and under various tilting angles, Tether Deployment Tests, under various temperatures, foldings and routings, Feet Sliding Resistance Tests, which determine the motion of the instrument in sand under inclined conditions on the Martian surface. The test setups and the results will be shown.

elib-URL des Eintrags:https://elib.dlr.de/106395/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Development of the Support System Used on the HP3 Instrument for Insight Mars Mission
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Reershemius, SieboSiebo.Reershemius (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Fittock, MarkMark.Fittock (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Spröwitz, TomTom.Sproewitz (at) dlr.dehttps://orcid.org/0000-0001-5369-6919NICHT SPEZIFIZIERT
Spohn, TilmanTilman.Spohn (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:2016
Referierte Publikation:Nein
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Insight, Mars Mission, HP3 instrument
Veranstaltungstitel:14th European Conference on Spacecraft Structures, Materials and Environmental Testing
Veranstaltungsort:Toulouse, France
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:27 September 2016
Veranstaltungsende:30 September 2016
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Technik für Raumfahrtsysteme
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R SY - Technik für Raumfahrtsysteme
DLR - Teilgebiet (Projekt, Vorhaben):R - Entfaltungstechnologie . Solar Sail (alt)
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme > Mechanik und Thermalsysteme
Hinterlegt von: Sznajder, Dr.-Ing. Maciej
Hinterlegt am:05 Okt 2016 15:06
Letzte Änderung:24 Apr 2024 20:11

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