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Simulation of the Separation Process of the SpaceLiner Booster from the SpaceLiner Passenger Stage

Stappert, Sven (2017) Simulation of the Separation Process of the SpaceLiner Booster from the SpaceLiner Passenger Stage. Project Report. SART TN-013/2017. 69 S.

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Abstract

The separation process of the SpaceLiner Booster from the SpaceLiner Passenger Stage is crucial for the success of the SpaceLiner’s mission and also for the passenger’s safety. Hence, a safe, clean, fast and reliable separation has to be guaranteed and proven. In this study, the multibody dynamics of the separation process have been investigated considering the use of solid propellant motors to accelerate the SpaceLiner Booster away from the Passenger Stage. Furthermore, critical failure modes have been simulated and identified and a baseline for the separation process has been defined.

Item URL in elib:https://elib.dlr.de/144105/
Document Type:Monograph (Project Report)
Additional Information:Das PDF ist auf Anfrage bei RY-SRT erhältlich!
Title:Simulation of the Separation Process of the SpaceLiner Booster from the SpaceLiner Passenger Stage
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Stappert, SvenUNSPECIFIEDhttps://orcid.org/0000-0002-8425-2779UNSPECIFIED
Date:September 2017
Refereed publication:No
Open Access:No
Number of Pages:69
Status:Published
Keywords:SpaceLiner, RLV, Separation, Multibody Dynamic Simulation, MBS
Department:RY-SRT
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Systems Analysis Space Transport (SART)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Vormschlag, Nele Marei
Deposited On:29 Sep 2021 12:20
Last Modified:29 Sep 2021 12:20

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