Simontacchia, Pamela und Sagnier, Sebastien und Edeline, Emmanuel und Blasi, Roland und Espinosa, Amaya und Caruana, Jean-Noël und Boujnah, Sandra und Altenhöfer, Philipp (2022) PROMETHEUS: PRECURSOR OF NEW LOW-COST ROCKET ENGINE FAMILY. In: Proceedings of the International Astronautical Congress, IAC. 73rd International Astronautical Congress, 2022-09-18 - 2022-09-22, Paris, France. ISSN 0074-1795.
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Offizielle URL: https://iac2022.org/
Kurzfassung
Prometheus is the precursor of a new European liquid rocket Engine family designed for low-cost, flexibility and reusability. This programme, initially undertaken through cooperation between the French national space agency CNES and ArianeGroup, entered in the ESA Future Launcher Preparatory Programme after the ESA Ministerial Conference in December 2016, with Germany, Italy, Belgium, Sweden and Switzerland joining France in the funding. A major aim of Prometheus project is to design, produce, and test an advanced low-cost 100-tons class LOx/LCH4 reusable Engine. This Engine, designed for 1MEuro recurrent cost, targets also flexibility in operation through variable thrust, multiple ignitions, compatibility to main and upper stage operation, and minimized ground operations before and after flight. To reach those ambitious objectives, an extreme design-to-cost approach is mandatory, as well as innovative technologies and advanced industrial capabilities; among the main levers, there are the extensive recourse to Additive Manufacturing for the production of engine components, the introduction of a full electric command system and the on-board Rocket Electronic Engine Computer (REEC) for Engine management and monitoring. In addition, Prometheus programme promotes the application of agile and frugal methodologies to get maximum benefit in product innovation and value creation in operation. This paper presents the global status of Prometheus advancements and gives a specific insight regarding the oncoming milestones: 2021 first engine delivery, 2022 engines tests realization on Themis 1G and engine test campaign preparation at P5 in DLR Lampoldshausen.
elib-URL des Eintrags: | https://elib.dlr.de/191445/ | ||||||||||||||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||||||||||
Titel: | PROMETHEUS: PRECURSOR OF NEW LOW-COST ROCKET ENGINE FAMILY | ||||||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | 2022 | ||||||||||||||||||||||||||||||||||||
Erschienen in: | Proceedings of the International Astronautical Congress, IAC | ||||||||||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||||||
In SCOPUS: | Ja | ||||||||||||||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||||||||||
ISSN: | 0074-1795 | ||||||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||||||
Stichwörter: | rocket engine test bench, space propulsion, PROMETEUS, LOX, methane, Themis, reusability, testing | ||||||||||||||||||||||||||||||||||||
Veranstaltungstitel: | 73rd International Astronautical Congress | ||||||||||||||||||||||||||||||||||||
Veranstaltungsort: | Paris, France | ||||||||||||||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||||||||||
Veranstaltungsbeginn: | 18 September 2022 | ||||||||||||||||||||||||||||||||||||
Veranstaltungsende: | 22 September 2022 | ||||||||||||||||||||||||||||||||||||
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 - Wiederverwendbare Raumfahrtsysteme und Antriebstechnologie | ||||||||||||||||||||||||||||||||||||
Standort: | Lampoldshausen | ||||||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe > Prüfstandtechnologie | ||||||||||||||||||||||||||||||||||||
Hinterlegt von: | Hanke, Michaela | ||||||||||||||||||||||||||||||||||||
Hinterlegt am: | 02 Dez 2022 08:08 | ||||||||||||||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:52 |
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