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Ariane 6 PPH Architecture Critical Analysis: Second Iteration Loop

Dumont, Etienne and Bozic, Ognjan and May, Stefan and Mierheim, Olaf and Chrupalla, David and Beyland, Lutz and Karl, Sebastian and Klevanski, J. and Johannsson, Magni and Clark, Vanessa and Stief, Malte and Keiderling, David and Koch, Patrick and Acquatella B., Paul and Saile, Dominik and Poppe, Georg and Traudt, Tobias and Manfletti, C. (2015) Ariane 6 PPH Architecture Critical Analysis: Second Iteration Loop. DLR-Forschungsbericht, DLR-Interner Bericht. X-TRAS TN-2015/013. DLR. 246 S. (Unpublished)

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Abstract

After a first critical analysis performed in 2013 on the first concept of the Ariane 6 PPH, a second iteration loop has been performed on the version of Ariane 6 PPH fixed in early 2014. The results of this Ariane 6 PPH architecture critical analysis are presented in this report. Compared to the configuration considered in 2013, the sizes of the stages have been increased to P145 and H32 for the P135 and the H30 respectively. This increase was indeed required to reach the target payload performance of 6.5 tons to GTO with sufficient margin. A preliminary model of the launcher with three P145 solid rocket motors (SRM) in the first stage, one identical P145 solid rocket motor in the second stage and a H32 cryogenic upper stage with separated tanks powered by Vinci was established. Subsequently, specific topics were analysed in more detail.

Item URL in elib:https://elib.dlr.de/95474/
Document Type:Monograph (DLR-Forschungsbericht, DLR-Interner Bericht)
Title:Ariane 6 PPH Architecture Critical Analysis: Second Iteration Loop
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Dumont, EtienneUNSPECIFIEDhttps://orcid.org/0000-0003-4618-0572UNSPECIFIED
Bozic, OgnjanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
May, StefanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Mierheim, OlafUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Chrupalla, DavidUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Beyland, LutzUNSPECIFIEDhttps://orcid.org/0000-0003-4885-1704UNSPECIFIED
Karl, SebastianUNSPECIFIEDhttps://orcid.org/0000-0002-5558-6673UNSPECIFIED
Klevanski, J.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Johannsson, MagniUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Clark, VanessaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Stief, MalteUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Keiderling, DavidUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Koch, PatrickUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Acquatella B., PaulUNSPECIFIEDhttps://orcid.org/0000-0002-0826-6984UNSPECIFIED
Saile, DominikUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Poppe, GeorgUNSPECIFIEDhttps://orcid.org/0000-0001-9003-3057UNSPECIFIED
Traudt, TobiasRA-RAK LAUNSPECIFIEDUNSPECIFIED
Manfletti, C.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:February 2015
Refereed publication:No
Open Access:No
Number of Pages:246
ISSN:0939-2963
Status:Unpublished
Keywords:Ariane 6, PPH, P145, European launcher, Vinci
Institution:DLR
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 - Projekt X-TRAS (old)
Location: Braunschweig , Bremen , Göttingen , Köln-Porz , Lampoldshausen , Oberpfaffenhofen
Institutes and Institutions:Institute of Space Systems
Institute of Space Propulsion
Institute of Composite Structures and Adaptive Systems
Institute of System Dynamics and Control
Institute of Aerodynamics and Flow Technology > Spacecraft
Institute of Aerodynamics and Flow Technology > Über- und Hyperschalltechnologien
Deposited By: Dumont, Etienne
Deposited On:02 Mar 2015 08:17
Last Modified:28 Mar 2023 23:43

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