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. Deutsches Zentrum für Luft- und Raumfahrt. (Unpublished)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:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
David, Emmanuelle	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Johannsson, Magni	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

November 2012

Refereed publication:

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

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Unpublished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 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:

Johannsson, Magni

Deposited On:

24 Apr 2014 10:39

Last Modified:

24 Apr 2014 10:39

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