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HEROS - Sounding Rocket Development by the HyEnD Project

Schmierer, Christian and Kobald, Mario and Tomilin, K. and Fischer, U. and Rehberger, M. and Schlechtriem, S. (2015) HEROS - Sounding Rocket Development by the HyEnD Project. 6th EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS), 29. Jun. - 03. Jul. 2015, Krakau, Polen.

Full text not available from this repository.

Abstract

The student team Hybrid Engine Development (HyEnD) of the University of Stuttgart is taking part with the Institute of Space Systems (IRS) in the DLR educational program STERN (Studentische Experimentalraketen). This program supports students at German universities to design, build and launch an experimental rocket within 3 years. HyEnD is developing a hybrid rocket called HEROS (Hybrid Experimental Rocket Stuttgart) with a thrust of 10 kN, a total impulse of over 100 kNs and an expected lift off weight up to 175 kg. HEROS is aimed to be launched in October 2015 from Esrange in Sweden to an expected flight altitude of 40 to 50 km. The current altitude record for amateur rockets in Europe is at approximately 12.5 km. HEROS’ hybrid rocket engine HyRES uses a paraffin-based solid fuel and nitrous oxide as the liquid oxidizer. In the course of the STERN program the student team not only has to master the difficulties of a high thrust hybrid rocket engine but also the development of a light weight oxidizer tank, valves, rocket structure, recovery system and electronics. Concluding, the development and construction of a lightweight hybrid sounding rocket for the given requirements and budget is described herein.

Item URL in elib:https://elib.dlr.de/99691/
Document Type:Conference or Workshop Item (Speech)
Title:HEROS - Sounding Rocket Development by the HyEnD Project
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Schmierer, ChristianChristian.Schmierer (at) dlr.deUNSPECIFIED
Kobald, MarioMario.Kobald (at) dlr.dehttps://orcid.org/0000-0002-1708-3944
Tomilin, K.Univ. StuttgartUNSPECIFIED
Fischer, U.Univ. StuttgartUNSPECIFIED
Rehberger, M.Markus.Rehberger (at) dlr.deUNSPECIFIED
Schlechtriem, S.Stefan.Schlechtriem (at) dlr.deUNSPECIFIED
Date:July 2015
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Hybridrakeketen, Paraffin, Lachgas, Sounding Rockets
Event Title:6th EUROPEAN CONFERENCE FOR AEROSPACE SCIENCES (EUCASS)
Event Location:Krakau, Polen
Event Type:international Conference
Event Dates:29. Jun. - 03. Jul. 2015
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Antriebsystemtechnik - Raketenantriebtests
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Propellants
Deposited By: Hanke, Michaela
Deposited On:23 Nov 2015 13:43
Last Modified:01 Dec 2018 19:51

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