elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Accessibility | Contact | Deutsch
Fontsize: [-] Text [+]

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

Rickmers, Peter and Kottmeier, Sebastian and Bauer, Waldemar and Delovski, Toni and Suhr, Birgit and 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.

[img] PDF - Only accessible within DLR
965kB

Abstract

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.

Item URL in elib:https://elib.dlr.de/188699/
Document Type:Conference or Workshop Item (Speech)
Title:The Reusability Flight Experiment - ReFEx: Agile AIV Processes for Prototype Flight Experiments
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Rickmers, PeterPeter.Rickmers (at) dlr.dehttps://orcid.org/0000-0001-6500-7922UNSPECIFIED
Kottmeier, SebastianSebastian.Kottmeier (at) dlr.dehttps://orcid.org/0000-0001-8129-1644UNSPECIFIED
Bauer, WaldemarWaldemar.Bauer (at) dlr.deUNSPECIFIEDUNSPECIFIED
Delovski, ToniToni.Delovski (at) dlr.deUNSPECIFIEDUNSPECIFIED
Suhr, BirgitBirgit.Suhr (at) dlr.deUNSPECIFIEDUNSPECIFIED
Klinkner, SabineUniversität Stuttgart, IRSUNSPECIFIEDUNSPECIFIED
Date:September 2022
Journal or Publication Title:73rd International Astronautical Congress, IAC 2022
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
ISSN:0074-1795
Status:Published
Keywords:RLV, hypersonic, flight experiment, AIV
Event Title:73rd International Astronautical Congress (IAC)
Event Location:Paris, Frankreich
Event Type:international Conference
Event Start Date:18 September 2022
Event End Date:22 September 2022
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Project ReFEx - Reusability Flight Experiment
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Systems Engineering and Project Office
Deposited By: Rickmers, Dr. Peter
Deposited On:06 Oct 2022 10:07
Last Modified:31 Oct 2024 10:06

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
OpenAIRE Validator logo electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.