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The Reusability Flight Experiment - ReFEx: Agile AIV Processes for Prototype Flight Experiments

Rickmers, Peter und Kottmeier, Sebastian und Bauer, Waldemar und Delovski, Toni und Suhr, Birgit und Klinkner, Sabine (2022) The Reusability Flight Experiment - ReFEx: Agile AIV Processes for Prototype Flight Experiments. In: 73rd International Astronautical Congress, IAC 2022. 73rd International Astronautical Congress (IAC), 2022-09-18 - 2022-09-22, Paris, Frankreich. ISSN 0074-1795.

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Kurzfassung

In November 2021 the ReFEx project passed the Critical Design Review (CDR) and is now in phase D. The experiment has been under development at the German Aerospace Center (DLR) since 2018 and is a technology demonstrator for aerodynamically controlled RLV stages. The experimental vehicle will be launched in 2024 on a VSB-30 sounding rocket, which injects ReFEx into a trajectory typical of such stages. The selected launch site is the Koonibba Test Range (KTR) in Southern Australia. Several key technologies required for future reusable stages that rely heavily on aerodynamic means of control will be tested. This includes the demonstration of a heading change of more than 30°, providing not only valuable flight data at the other end of the spectrum for RLVs (Reusable Launch Vehicle) from propulsive return flights [1], but also added capability with very flexible divert capabilities. To be able to use the VSB-30 the vehicle needed to be compact to remain within the limited volume available. As such it has a length of 2.7 m, a wingspan of 1.1 m, a mass of approx. 400 kg and is very densely packed with internal systems [1]. This paper provides an update of the flight experiment and focuses on the Assembly Integration and Verification (AIV) methods used. Key challenges in this regard are the employed model philosophies and corresponding validation steps. The hybrid approach taken could be an interesting template for other flight experiments aiming to strike a balance between suitable reliability and the unknowns of a prototype technology demonstrator. To aid in this the AIV processes are augmented with a novel information management system, robotically assisted integration, core avionics test benches and augmented reality applications. ReFEx is the first flight system to be assembled in the DLR Bremen making use of these new approaches. As such the processes will be monitored throughout against key performance indicators to improve process efficiency for future projects.

elib-URL des Eintrags:https://elib.dlr.de/188699/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:The Reusability Flight Experiment - ReFEx: Agile AIV Processes for Prototype Flight Experiments
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Rickmers, PeterPeter.Rickmers (at) dlr.dehttps://orcid.org/0000-0001-6500-7922NICHT SPEZIFIZIERT
Kottmeier, SebastianSebastian.Kottmeier (at) dlr.dehttps://orcid.org/0000-0001-8129-1644NICHT SPEZIFIZIERT
Bauer, WaldemarWaldemar.Bauer (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Delovski, ToniToni.Delovski (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Suhr, BirgitBirgit.Suhr (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Klinkner, SabineUniversität Stuttgart, IRSNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:September 2022
Erschienen in:73rd International Astronautical Congress, IAC 2022
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Nein
ISSN:0074-1795
Status:veröffentlicht
Stichwörter:RLV, hypersonic, flight experiment, AIV
Veranstaltungstitel:73rd International Astronautical Congress (IAC)
Veranstaltungsort:Paris, Frankreich
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:18 September 2022
Veranstaltungsende:22 September 2022
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 - Projekt ReFEx - Reusability Flight Experiment
Standort: Bremen
Institute & Einrichtungen:Institut für Raumfahrtsysteme > Systementwicklung und Projektbüro
Hinterlegt von: Rickmers, Dr. Peter
Hinterlegt am:06 Okt 2022 10:07
Letzte Änderung:31 Okt 2024 10:06

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