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Size Matters - The Shell Lander Concept for Exploring Medium-Size Airless Bodies

Grimm, Christian und Schröder, Silvio und Witte, Lars und Wickhusen, Kai (2018) Size Matters - The Shell Lander Concept for Exploring Medium-Size Airless Bodies. In: 69th International Astronautical Congress 2018, IAC 2018. 69th International Astronautical Congress (IAC), 2018-10-01 - 2018-10-05, Bremen, Germany.

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Kurzfassung

Once addressed as a side topic in planetary exploration, the investigation of small solar system bodies has now become one of the corner stones in the international science community in order to study the formation of the solar system and the evolution of life within. For rendezvous spacecraft, small carry-on landers have proven to be valuable assets, and to have a positive impact on the overall mission cost, by avoiding additional complexity of the main satellite and transferring the risk of close surface maneuvers entirely or at least to some extend to an independent deployable system. However, carry-on landers have been designed currently to land on very small bodies only, but medium-size class objects between diameters of 10 - 50 km are of great interest as well. In this paper we classify carry-on landers with respect to their touchdown and operational strategy, evaluate the constraints of ballistic deployments for different target bodies as well as identify the niche for using simple honeycomb impact dampers compared to optional retro-propulsion systems. Further we introduce the system design of a guided Shell Lander using a generic instrument carrier attached to a single ejectable crash-pad with stabilizing capability to protect the instrument carrier from structural damage, limit internal shock loads for sensitive payloads as well as reduce the amount of bounces on the surface. Finally, we present a mission architecture for a reference case to the Martian moon Phobos as well as provide a proof of concept based on laboratory impact tests.

elib-URL des Eintrags:https://elib.dlr.de/122161/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Size Matters - The Shell Lander Concept for Exploring Medium-Size Airless Bodies
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Grimm, Christianchristian.grimm (at) dlr.dehttps://orcid.org/0000-0003-4490-7424NICHT SPEZIFIZIERT
Schröder, SilvioSilvio.Schroeder (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Witte, LarsLars.Witte (at) dlr.dehttps://orcid.org/0000-0002-3921-2524NICHT SPEZIFIZIERT
Wickhusen, Kaikai.wickhusen (at) dlr.dehttps://orcid.org/0000-0003-2524-5285NICHT SPEZIFIZIERT
Datum:1 Oktober 2018
Erschienen in:69th International Astronautical Congress 2018, IAC 2018
Referierte Publikation:Nein
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Asteroid Landing, Payload Delivery, Impact Energy Absorption, Shell Lander, Ejectable Crash-Pad
Veranstaltungstitel:69th International Astronautical Congress (IAC)
Veranstaltungsort:Bremen, Germany
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:1 Oktober 2018
Veranstaltungsende:5 Oktober 2018
Veranstalter :IAF
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Erforschung des Weltraums
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R EW - Erforschung des Weltraums
DLR - Teilgebiet (Projekt, Vorhaben):R - Vorhaben Landetechnologien (alt)
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme > Land und Explorationstechnologie
Hinterlegt von: Grimm, Christian
Hinterlegt am:13 Okt 2018 12:42
Letzte Änderung:24 Apr 2024 20:26

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