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

LUMEN: Putting into Operation a Flexible Test Bed for Next-Generation Rocket Engine Technologies

Traudt, Tobias and Börner, Michael and Armbruster, Wolfgang and Dos Santos Hahn, Robson Henrique and Dresia, Kai and Kurudzija, Eldin and Groll, Christopher and Müller, Max Axel and Klein, Sebastian and Haemisch, Jan and Deeken, Jan C. and Suslov, Dmitry and Hardi, Justin and Schlechtriem, Stefan (2025) LUMEN: Putting into Operation a Flexible Test Bed for Next-Generation Rocket Engine Technologies. In: 35th International Symposium on Space Technology and Science ISTS. 35th International Symposium on Space Technology and Science ISTS, 2025-07-12 - 2025-07-18, Tokusima, Japan.

[img] PDF - Only accessible within DLR
949kB

Abstract

In 2024, the German Aerospace Centre (DLR) successfully completed the hot-fire testing of the Liquid Upper Stage Demonstrator Engine (LUMEN), marking the final milestone in developing DLR's first rocket engine. LUMEN is an experimental expander-bleed cycle rocket engine that uses liquid oxygen (LOX) and liquefied natural gas (LNG) as propellants, generating 25 kN of thrust. With this achievement, LUMEN is now fully operational and available as a test bed for advanced technology development, such as intelligent engine control. LUMEN’s open research platform, free from external intellectual property restrictions, enables DLR to offer it as a testing platform to interested partners both domestically and internationally. Its modular design allows for component evaluations in a realistic environment, and the engine as a whole can support the development of engine-related technologies that would otherwise be challenging to test. After the initial tests of LUMEN, a subsequent test campaign was conducted with a focus on operating the engine as a research test bed. LUMEN was also used to demonstrate the intelligent control with a neural network controller. To establish a baseline design for the next step in intelligent control, some improvements are implemented. A new LOX impeller in the Oxygen Turbopump (OTP) provides a higher efficiency, while the cycle is optimized by reducing pressure losses throughout the system by removing two valves and introducing a newly optimized injector head. The new injector head uses shear coaxial elements in the outer row and swirl elements in the inner row, which not only reduce pressure losses but also enhance flame anchoring and heat transfer. Furthermore, the chilldown time was shortened to reduce the amount of propellant necessary for engine cooling while simultaneously deepening the understanding of chilldown prediction. Both, the operation time and the overall system efficiency were significantly improved during this campaign. The results of these tests will be presented in this paper.

Item URL in elib:https://elib.dlr.de/218874/
Document Type:Conference or Workshop Item (Speech)
Title:LUMEN: Putting into Operation a Flexible Test Bed for Next-Generation Rocket Engine Technologies
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Traudt, TobiasUNSPECIFIEDhttps://orcid.org/0000-0002-0206-0483196794895
Börner, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-3441-2869196794896
Armbruster, WolfgangUNSPECIFIEDhttps://orcid.org/0000-0002-4859-4173196794897
Dos Santos Hahn, Robson HenriqueUNSPECIFIEDhttps://orcid.org/0000-0002-2389-2043UNSPECIFIED
Dresia, KaiUNSPECIFIEDhttps://orcid.org/0000-0003-3229-5184UNSPECIFIED
Kurudzija, EldinUNSPECIFIEDhttps://orcid.org/0000-0001-5409-3845UNSPECIFIED
Groll, ChristopherUNSPECIFIEDhttps://orcid.org/0000-0001-9183-7081196794898
Müller, Max AxelUNSPECIFIEDhttps://orcid.org/0009-0007-2701-310X196794900
Klein, SebastianUNSPECIFIEDhttps://orcid.org/0000-0002-0579-655XUNSPECIFIED
Haemisch, JanUNSPECIFIEDhttps://orcid.org/0000-0001-9463-1740UNSPECIFIED
Deeken, Jan C.UNSPECIFIEDhttps://orcid.org/0000-0002-5714-8845UNSPECIFIED
Suslov, DmitryUNSPECIFIEDhttps://orcid.org/0000-0002-5160-9292UNSPECIFIED
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261UNSPECIFIED
Schlechtriem, StefanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2025
Journal or Publication Title:35th International Symposium on Space Technology and Science ISTS
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:International Symposium on Space Technology and Science ISTS
Status:Published
Keywords:LUMEN, rocket engine, LOX/LNG, turbopump, intelligent control
Event Title:35th International Symposium on Space Technology and Science ISTS
Event Location:Tokusima, Japan
Event Type:international Conference
Event Start Date:12 July 2025
Event End Date:18 July 2025
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 LUMEN (Liquid Upper Stage Demonstrator Engine), R - Reusable Space Systems and Propulsion Technology
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Engine Systems
Institute of Space Propulsion > Rocket Propulsion Technology
Institute of Space Propulsion > Leitungsbereich RA
Institute of Space Propulsion > Applied Hydrogen Technologies
Deposited By: Traudt, Tobias
Deposited On:13 Nov 2025 08:04
Last Modified:13 Nov 2025 08:04

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.