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Next Generation Launcher-Potential Ariane 5ME and Ariane 6 Common Upper Stage Options

David, Emmanuelle and Johannsson, Magni (2012) Next Generation Launcher-Potential Ariane 5ME and Ariane 6 Common Upper Stage Options. DLR-Interner Bericht. (Unpublished)

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Abstract

This study compares the performances of Ariane 5ME and Ariane 6 (for two different configurations: PPH and PH) with common upper stages. In that perspective, the investigated upper stages are ESC-B (Perigee Decrease and Direct Deorbiting Versions) and newly defined H31 and H34. Ariane 6 is modeled based on one or two P135 stages (serial) and similarly, two P135 boosters.

Item URL in elib:https://elib.dlr.de/88883/
Document Type:Monograph (DLR-Interner Bericht)
Title:Next Generation Launcher-Potential Ariane 5ME and Ariane 6 Common Upper Stage Options
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
David, Emmanuelleemmanuelle.david (at) dlr.deUNSPECIFIED
Johannsson, Magnimagni.johannsson (at) dlr.deUNSPECIFIED
Date:November 2012
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Unpublished
Keywords:Upper Stage, ESC-B, H31, H34, GTO, Ariane 5 ME, Ariane 6
Institution:Deutsches Zentrum für Luft- und Raumfahrt
Department:Systemanalyse Raumtransport
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: Johannsson, Magni
Deposited On:24 Apr 2014 10:39
Last Modified:24 Apr 2014 10:39

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