elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Kontakt | English
Schriftgröße: [-] Text [+]

Evaluation of Future Ariane Reusable VTOL Booster stages

Dumont, Etienne und Stappert, Sven und Ecker, Tobias und Wilken, Jascha und Karl, Sebastian und Krummen, Sven und Sippel, Martin (2017) Evaluation of Future Ariane Reusable VTOL Booster stages. In: Proceedings of the International Astronautical Congress, IAC. 68th International Astronautical Congress, 2017-09-25 - 2017-09-29, Adelaide, Australia.

[img] PDF (IAC Paper)
948kB
[img] PDF (IAC Presentation)
1MB

Kurzfassung

Reusability is anticipated to strongly impact the launch service market if sufficient reliability and low refurbishment costs can be achieved. DLR is performing an extensive study on return methods for a reusable booster stage for a future launch vehicle. The present study focuses on the vertical take-off and vertical landing (VTOL) method. First, a restitution of a flight of Falcon 9 is presented in order to assess the accuracy of the tools used. Then, the preliminary designs of different variants of a future Ariane launch vehicle with a reusable VTOL booster stage are described. The proposed launch vehicle is capable of launching a seven ton satellite into a geostationary transfer orbit (GTO) from the European spaceport in Kourou. Different stagings and propellants (LOx/LH2, LOx/LCH4, LOx/LC3H8, subcooled LOx/LCH4) are considered, evaluated and compared. First sizing of a broad range of launcher versions are based on structural index derived from existing stages. Ascent and descent trajectories of the first stage are optimized together in order to reach the highest payload while keeping mechanical loads at reasonable levels. Another important aspect is the aerothermal environment stressing the structure. During the re-entry boost, the first stage is immersed in the engine exhaust plume. Steady state computational fluid dynamics calculations are performed along the re-entry trajectory to characterise the flow field during retro-propulsion around the first stage. The resulting aerothermal database is coupled with a simple structural model to study the time dependent heating of the hull structure. Based on these first iteration results more detailed preliminary designs are performed in a second iteration for selected configurations: a LOx/LH2 launcher and a LOx/LCH4 launcher both equipped with gas generator engines.

elib-URL des Eintrags:https://elib.dlr.de/114430/
Dokumentart:Konferenzbeitrag (Vortrag)
Zusätzliche Informationen:IAC-17-D2.4.3
Titel:Evaluation of Future Ariane Reusable VTOL Booster stages
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Dumont, Etienneetienne.dumont (at) dlr.dehttps://orcid.org/0000-0003-4618-0572NICHT SPEZIFIZIERT
Stappert, Svensven.stappert (at) dlr.dehttps://orcid.org/0000-0002-8425-2779NICHT SPEZIFIZIERT
Ecker, TobiasTobias.Ecker (at) dlr.dehttps://orcid.org/0000-0001-7134-1185NICHT SPEZIFIZIERT
Wilken, JaschaJascha.Wilken (at) dlr.dehttps://orcid.org/0000-0001-5748-1261NICHT SPEZIFIZIERT
Karl, Sebastiansebastian.karl (at) dlr.dehttps://orcid.org/0000-0002-5558-6673NICHT SPEZIFIZIERT
Krummen, Svensven.krummen (at) dlr.dehttps://orcid.org/0000-0002-4126-688XNICHT SPEZIFIZIERT
Sippel, Martinmartin.sippel (at) dlr.dehttps://orcid.org/0000-0001-7356-7575NICHT SPEZIFIZIERT
Datum:27 September 2017
Erschienen in:Proceedings of the International Astronautical Congress, IAC
Referierte Publikation:Nein
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Ariane, reusability, toss-back, vertical landing, VTOL, VTVL, liquid hydrogen, liquid oxygen, liquid methane, liquid propane, subcooled methane, gas generator, staged combustion, RTLS, DRL
Veranstaltungstitel:68th International Astronautical Congress
Veranstaltungsort:Adelaide, Australia
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:25 September 2017
Veranstaltungsende:29 September 2017
Veranstalter :IAF
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - Raumfahrzeugsysteme - Systemanalyse Raumtransport (alt)
Standort: Bremen , Göttingen
Institute & Einrichtungen:Institut für Raumfahrtsysteme > Systemanalyse Raumtransport
Institut für Aerodynamik und Strömungstechnik > Raumfahrzeuge, GO
Hinterlegt von: Dumont, Etienne
Hinterlegt am:28 Sep 2017 11:14
Letzte Änderung:24 Apr 2024 20:18

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.