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

Current status of the DLR Reusability Flight Experiment - ReFEx

Rickmers, Peter und Bauer, Waldemar und Stappert, Sven und Kiehn, Daniel und Sippel, Martin (2018) Current status of the DLR Reusability Flight Experiment - ReFEx. HiSST: International Conference on High-Speed Vehicle Science Technology, 2018-11-26 - 2018-11-29, Moskau.

[img] PDF - Nur DLR-intern zugänglich
870kB

Kurzfassung

The Reusability Flight Experiment (ReFEx) is being developed by DLR (German Aerospace Center) to provide flight and design data on, as well as operational experience with, a winged first stage of a reusable launch vehicle (RLV). As such ReFEx will be a small technology demonstrator and is slated for launch in 2021. The experiment will be launched on a VSB-30 sounding rocket to altitudes and velocities similar to a first staging event and will then attempt a return flight along a trajectory comparable to a returning winged first stage RLV, transitioning from hypersonic speeds down to subsonic flight. ReFEx is about 2.7 m in length, has a wingspan of about 1.1 m and has a mass of approx. 450kg. It is controlled by a nitrogen cold gas reaction system (RCS) while outside the atmosphere and shall transition to aerodynamic control surfaces (canards and rudder) when atmospheric effects come into play. The maximum Mach number reached during the re-entry manoeuvre is about Mach 5. Besides being able to fly an optimised trajectory (generated autonomously on-board) to reduce the thermal and mechanical loads, ReFEx shall demonstrate manoeuvrability by flying a turn of at least 30° with respect to the original heading measured from entry interface. The entry interface was placed at 60 km altitude for the purposes of this experiment, as the effects of the atmosphere become significant at this altitude for the foreseen trajectory. The key technologies demonstrated in this vehicle are, amongst others: aerodynamic design of a vehicle capable of stable flight through many flow regimes, guidance, navigation and control (GNC) capable of on board generation of an optimised trajectory, the seamless transition between extraand intra-atmospheric flight controls and health monitoring of the vehicle status during flight using advanced sensors such as Fiber Optic Sensors (FOS) and Flush Air Data System (FADS). There has been an extensive planning phase for ReFEx and it has successfully passed SRR (Systems Requirements Review) and entered phase B development in February of 2018. ReFEx is one of the largest flight experiments conducted at DLR and officially became a fully funded project in April of 2018. This paper will give an overview of the current technological as well as the project status and provide some more detailed analysis on the re-entry scenarios studied for the mission.

elib-URL des Eintrags:https://elib.dlr.de/126516/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Current status of the DLR Reusability Flight Experiment - ReFEx
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Rickmers, PeterPeter.Rickmers (at) dlr.dehttps://orcid.org/0000-0001-6500-7922NICHT SPEZIFIZIERT
Bauer, Waldemarwaldemar.bauer (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Stappert, SvenSven.Stappert (at) dlr.dehttps://orcid.org/0000-0002-8425-2779NICHT SPEZIFIZIERT
Kiehn, DanielDaniel.Kiehn (at) dlr.dehttps://orcid.org/0000-0001-7383-0740NICHT SPEZIFIZIERT
Sippel, Martinmartin.sippel (at) dlr.dehttps://orcid.org/0000-0001-7356-7575NICHT SPEZIFIZIERT
Datum:November 2018
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:reusable launch vehicles, flight experiment, technology demonstrator
Veranstaltungstitel:HiSST: International Conference on High-Speed Vehicle Science Technology
Veranstaltungsort:Moskau
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:26 November 2018
Veranstaltungsende:29 November 2018
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
Institut für Raumfahrtsysteme > Systemanalyse Raumtransport
Hinterlegt von: Rickmers, Dr. Peter
Hinterlegt am:20 Feb 2019 09:38
Letzte Änderung:24 Apr 2024 20:30

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.