Johannsson, Magni und Dumont, Etienne und Clark, Vanessa und David, Emmanuelle und Sippel, Martin (2016) Launcher Pre-Design: ANGELA: A Next GEneration LAuncher - Trajectory and Payload Optimisation. Projektbericht. SART TN006/2013. DLR: Institut für Raumfahrtsysteme. 104 S. (nicht veröffentlicht)
Dieses Archiv kann nicht den Volltext zur Verfügung stellen.
Kurzfassung
This technical report describes the methodology used and the results of the preliminary design of four launcher configurations studied by DLR’s Space Launcher System Analysis division (SART) in Bremen, Germany, in the ANGELA project started in 2012. In the frame of this project funded by DLR-RfM and led by EADS Astrium, with cooperation of MT Aerospace, MBDA Bayern Chemie and Astos Solutions, DLR-SART performed the sizing and staging of four launch vehicle configurations with the capability to inject payloads in the range between 2 and 5 tons to GTO (Geostationary Transfer Orbit). Two HH and two Multi-PH configurations with various numbers of solid boosters are considered. For each launcher the optimisation of the staging is explained and sensitivity analysis results are given. These sensitivity analyses were a prerequisite for a good preparation of the Concurrent Engineering (CE) studies which followed the preliminary design optimisation. The resulting launcher configurations are: • 2 to 6 P36, H110 with 2 shortened Vulcain 2 and H29 with Vinci • 2 to 6 P34, H90 with a new high thrust staged combustion engine and H24 with Vinci • 2 or 3 P120, P120 and H23 with Vinci • 2 or 3 P110, P110 and H23 with Vinci
elib-URL des Eintrags: | https://elib.dlr.de/107462/ | ||||||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Dokumentart: | Berichtsreihe (Projektbericht) | ||||||||||||||||||||||||
Titel: | Launcher Pre-Design: ANGELA: A Next GEneration LAuncher - Trajectory and Payload Optimisation | ||||||||||||||||||||||||
Autoren: |
| ||||||||||||||||||||||||
Datum: | 2016 | ||||||||||||||||||||||||
Referierte Publikation: | Nein | ||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||
Seitenanzahl: | 104 | ||||||||||||||||||||||||
Status: | nicht veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | New Generation Launcher, Ariane 6, Cryogenic Upper Stage, Vulcain 2, Vinci, Vega, Multi-PH, 2PPH, 3PPH, PPH, HH, Staged combustion Engine, SRM, Trajectory analysis, Performance, Optimisation, Sensitivity | ||||||||||||||||||||||||
Institution: | DLR: Institut für Raumfahrtsysteme | ||||||||||||||||||||||||
Abteilung: | Systemanalyse Raumtransport | ||||||||||||||||||||||||
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 | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtsysteme > Systemanalyse Raumtransport | ||||||||||||||||||||||||
Hinterlegt von: | Dumont, Etienne | ||||||||||||||||||||||||
Hinterlegt am: | 09 Nov 2016 09:42 | ||||||||||||||||||||||||
Letzte Änderung: | 13 Jun 2018 11:39 |
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags