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Preliminary Design and Development of MAST, a Multivehicle Analysis and Separation Tool

Gäßler, Björn and Acquatella B., Paul and Yábar Vallès, Cèlia and Rinalducci, Antonio and Bennani, Samir (2021) Preliminary Design and Development of MAST, a Multivehicle Analysis and Separation Tool. 8th International Conference on Astrodynamics Tools and Techniques, 23.-25. Jun. 2021, Online.

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Abstract

The recent surge in demand for launch opportunities of multiple small satellites has stimulated further development of dedicated dispensers and new multi-payload concepts. A large market of adapters and deployment technologies has been created to compactly house future small satellites on existing launchers. However, these new launch scenarios come with a new set of challenges and requirements regarding satellite separation dynamics which are very particular to each dedicated mission or dispenser. Separation dynamics modeling in a multi-body simulation environment is therefore a critical capability to develop regarding those future mission scenarios. This motivates the objective of this paper which is to present the preliminary design and development of a dedicated multi-body dynamics simulation tool denominated MAST (Multivehicle Analysis and Separation Tool) to provide the means to verify the required separation requirements and to verify absence of collisions between the separated satellites and the upper stage during the separation processes. The implementation of this tool and a test-case are presented together with some results from a realistic use-case scenario involving a hypothetical VEGA SMSS flight mission. This preliminary design and development of MAST shows satisfying results in terms of the tool's requirements also briefly outlined in the paper as well as its potential to assist in future launch scenarios involving multivehicle separations.

Item URL in elib:https://elib.dlr.de/143559/
Document Type:Conference or Workshop Item (Speech)
Title:Preliminary Design and Development of MAST, a Multivehicle Analysis and Separation Tool
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Gäßler, BjörnBjoern.Gaessler (at) dlr.deUNSPECIFIED
Acquatella B., PaulPaul.Acquatella (at) dlr.dehttps://orcid.org/0000-0002-0826-6984
Yábar Vallès, CèliaEuropean Space AgencyUNSPECIFIED
Rinalducci, AntonioEuropean Space AgencyUNSPECIFIED
Bennani, SamirEuropean Space AgencyUNSPECIFIED
Date:June 2021
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Multi-physics modeling, payload separation, launcher systems, multi-domain modeling, multibody dynamics, Simscape
Event Title:8th International Conference on Astrodynamics Tools and Techniques
Event Location:Online
Event Type:international Conference
Event Dates:23.-25. Jun. 2021
Organizer:ESA, NASA, JAXA, DLR, CNES, ASI, TsAGI, UKSA, and ROSA
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Research under Space Conditions
DLR - Research area:Raumfahrt
DLR - Program:R FR - Research under Space Conditions
DLR - Research theme (Project):R - Model systems
Location: Oberpfaffenhofen
Institutes and Institutions:Institute of System Dynamics and Control
Deposited By: Gäßler, Björn
Deposited On:25 Oct 2021 09:57
Last Modified:25 Oct 2021 09:57

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