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HYDRA III Hybrid Rocket Engine - Flight Version Test Results

Hink, Rüdiger (2015) HYDRA III Hybrid Rocket Engine - Flight Version Test Results. In: Deutscher Luft- und Raumfahrtkongress 2015. DGLR. Deutscher Luft- und Raumfahrtkongress 2015, 2015-09-22 - 2015-09-24, Rostock, Deutschland.

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Official URL: http://www.dlrk2015.dglr.de/


The flight version of the HYDRA III hybrid rocket engine was built by the ExperimentalRaumfahrt-InteressenGemeinschaft e.V. (ERIG) in cooperation with the Institute of Aerospace Systems of TU Braunschweig. The HYDRA III engine was improved to a thrust of about 1300 N for the supersonic rocket named FAUST of the Studentische Experimental-Raketen program (STERN), which is initiated by the German Aerospace center (DLR). The launch of the FAUST rocket is planned to be at the end of this year at the Esrange Space Center in Kiruna (North Sweden). The aim of the STERN program is to motivate and educate students for aerospace sciences by developing a rocket. The ERIG advanced therefore the hybrid rocket engine HYDRA III, which bases on a liquid oxidizer and a solid fuel grain as propellants. Therefore, liquid nitrous oxide is used as oxidizer and hydroxyl-terminated polybutadiene (HTPB) with metal powder as solid fuel grain. For the flight version of this engine a carbon fiber reinforced plastic (CFRP) oxidizer vessel and the CFRP flight pressure vessel with helium were used. Also a new lightweight flight version valve segment was used to control the high amount of oxidizer mass flow into the combustion chamber. The latest test results of this flight engine from the horizontal test bench as well as the set-up of the vertical test bench are presented.

Item URL in elib:https://elib.dlr.de/97794/
Document Type:Conference or Workshop Item (Speech)
Title:HYDRA III Hybrid Rocket Engine - Flight Version Test Results
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Journal or Publication Title:Deutscher Luft- und Raumfahrtkongress 2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:Hybrid Rocket Engine, STERN program
Event Title:Deutscher Luft- und Raumfahrtkongress 2015
Event Location:Rostock, Deutschland
Event Type:national Conference
Event Start Date:22 September 2015
Event End Date:24 September 2015
Organizer:Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.
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 - Vorhaben AHRES (old)
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Hink, Rüdiger Reiner
Deposited On:15 Oct 2015 11:47
Last Modified:24 Apr 2024 20:03

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