Clark, Vanessa Jane (2014) Ariane 6 Upper Stage Deorbitation. Other. SART TN-015/2014. Other. DLR. (Unpublished)
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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/ | ||||||||
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Document Type: | Monograph (Other, Other) | ||||||||
Additional Information: | .pdf auf Anfrage bei RY-SRT erhältlich! | ||||||||
Title: | Ariane 6 Upper Stage Deorbitation | ||||||||
Authors: |
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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Status: | Unpublished | ||||||||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 Transportation | ||||||||
DLR - Research area: | Raumfahrt | ||||||||
DLR - Program: | R RP - Space Transportation | ||||||||
DLR - Research theme (Project): | R - Raumfahrzeugsysteme - Systemanalyse Raumtransport (old) | ||||||||
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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