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Ariane 6 Upper Stage Deorbitation

Clark, Vanessa Jane (2014) Ariane 6 Upper Stage Deorbitation. Other. Other. SART TN-015/2014. (Unpublished)

Full text not available from this repository.

Abstract

As part of Ariane 6 development activities, compliance with Space Debris Requirements is being demonstrated. This report focusses one aspect of the compliance: “R9- Operational Requirements: Launcher stages shall satisfy one of the following conditions: a) A direct re-entry shall be performed as part of the launcher sequence” Various deorbitation scenarios were investigated, and an optimal re-entry strategy concerning flexibility and mass penalty was selected to be: • Boost performed by Vinci engine at 90 kN, • 3600 s coast time, • Burn angle 120o, and • ΔV 60 m/s. The propellant budget for this manoeuvre was found to be 403 kg (including reserves and 20% margin). The modelling of the direct (controlled) deorbit of the Ariane 6 Upper Stage was performed using the ESA software DRAMA and the DLR-SART software tool dust.

Item URL in elib:https://elib.dlr.de/111433/
Document Type:Monograph (Other, Other)
Additional Information:.pdf auf Anfrage bei RY-SRT erhältlich!
Title:Ariane 6 Upper Stage Deorbitation
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Clark, Vanessa JaneDLRUNSPECIFIED
Date:8 August 2014
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:Ariane 6, Debris Mitigation, Upper Stage, Direct Deorbitation, Geostationary Transfer Orbit (GTO)
Institution:DLR
Department:RY-SRT
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Systemanalyse Raumtransport
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Vormschlag, Nele Marei
Deposited On:09 Mar 2017 09:58
Last Modified:09 Mar 2017 09:58

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