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MMX Rover MECSS - Separation from the Mothership: Multibody Simulation Analysis of the Ejection

Pignede, Antoine Francois Xavier and Buse, Fabian and Grundmann, Jan Thimo and Reershemius, Siebo and Patscheider, Hagen and Wippermann, Torben and Lange, Michael and Mierheim, Olaf and Meyer, Sebastian (2025) MMX Rover MECSS - Separation from the Mothership: Multibody Simulation Analysis of the Ejection. Multibody System Dynamics. Springer. doi: 10.1007/s11044-025-10076-y. ISSN 1384-5640.

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Official URL: https://link.springer.com/article/10.1007/s11044-025-10076-y

Abstract

This is a report about the simulation study of a lightweight rover being separated from a larger spacecraft in vicinity of a small Solar system body. Monte Carlo simulation and statistical analysis estimate the rate of requirement violation depending on uncertain rover and separation mechanism parameters. During the rover development phase, the full Monte Carlo analysis is only done with a simplified model. The first iterations show relatively high probability of non-compliance with requirements. Model refinement and more precise hardware values lead to the final assessment that separation meets the requirements within a 2 sigma region. A more detailed model serves for analysis of selected samples during the development phase. For this model, a full Monte Carlo analysis is only done close to the end once the parameter ranges are fixed, mostly for time reasons. This more detailed analysis in general confirms the 2 sigma requirement meeting. The main difference with the simplified model is the much larger number of outliers, a few of which also violate the allocated volume for the rover in proximity of the mothership.

Item URL in elib:https://elib.dlr.de/213990/
Document Type:Article
Title:MMX Rover MECSS - Separation from the Mothership: Multibody Simulation Analysis of the Ejection
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Pignede, Antoine Francois XavierAntoine.Pignede (at) dlr.dehttps://orcid.org/0000-0002-9255-2405UNSPECIFIED
Buse, FabianFabian.Buse (at) dlr.dehttps://orcid.org/0000-0002-2279-5735UNSPECIFIED
Grundmann, Jan ThimoJan.Grundmann (at) dlr.deUNSPECIFIEDUNSPECIFIED
Reershemius, SieboSiebo.Reershemius (at) dlr.deUNSPECIFIEDUNSPECIFIED
Patscheider, HagenHagen.Patscheider (at) dlr.deUNSPECIFIEDUNSPECIFIED
Wippermann, TorbenTorben.Wippermann (at) dlr.dehttps://orcid.org/0000-0002-0354-6557UNSPECIFIED
Lange, MichaelM.Lange (at) dlr.dehttps://orcid.org/0000-0003-0095-3605UNSPECIFIED
Mierheim, OlafOlaf.Mierheim (at) dlr.deUNSPECIFIEDUNSPECIFIED
Meyer, SebastianSebastian.Meyer (at) dlr.dehttps://orcid.org/0009-0001-8113-1330183444649
Date:18 April 2025
Journal or Publication Title:Multibody System Dynamics
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
DOI:10.1007/s11044-025-10076-y
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
Negrut, DanUniversity of Wisconsin-MadisonUNSPECIFIEDUNSPECIFIED
Serban, RaduUniversity of Wisconsin-MadisonUNSPECIFIEDUNSPECIFIED
Mikkola, AkiLUT UniversityUNSPECIFIEDUNSPECIFIED
Publisher:Springer
Series Name:Advances in Multibody System Dynamics
ISSN:1384-5640
Status:Published
Keywords:Monte Carlo analysis, Small celestial bodies, MMX, Modeling and simulation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space System Technology
DLR - Research area:Raumfahrt
DLR - Program:R SY - Space System Technology
DLR - Research theme (Project):R - Project MMX [SY], R - Project MMX [RO]
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of Space Systems > Systems Engineering and Project Office
Institut für Systemleichtbau > Composite Design
Institute of Space Systems > Quality Management and Product Assurance for Space Systems
Institute of Robotics and Mechatronics (since 2013) > System Dynamics
Deposited By: Pignede, Antoine Francois Xavier
Deposited On:20 May 2025 12:02
Last Modified:20 May 2025 12:02

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