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A Record Flight of the Hybrid Sounding Rocket HEROS 3

Kobald, Mario and Schmierer, C. and Fischer, U. and Tomilin, K. and Petrarolo, Anna (2017) A Record Flight of the Hybrid Sounding Rocket HEROS 3. 31st International Symposium on Space Technology and Science (ISTS), 3.-9. Jun. 2017, Matsuyama, Japan.

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Abstract

Hybrid rocket propulsion offers inherent safety during handling and launch operations at low cost. This makes it not only attractive for space tourism applications like SpaceShipTwo but also for sounding rockets and for educational activities with students. This has been successfully demonstrated by the HyEnD student project from the University of Stuttgart: On November 8th, 2016 at 10:30 a.m. the hybrid sounding rocket HEROS 3 was launched from the Esrange Space Center to an apogee altitude of 32,300m (106,000 ft). This set a new altitude record for European student and amateur rocketry. Furthermore, this is a world altitude record for hybrid rockets built by students. It was successfully recovered with the drogue and main parachute being released. The rocket was powered by a 10 kN design thrust hybrid rocket engine with a paraffin-based fuel and Nitrous Oxide (N2O) as the oxidizer. The combustion efficiency was verified to be above 97% in ground tests. Liquid burn time in the flight was for 15 s with an additional combustion of gaseous N2O in the blow-down mode of about 10 s. The rocket was 7.5m long with an empty mass of about 75 kg. The rocket structure was made completely from light-weight carbon fibre and glass fibre reinforced plastic.

Item URL in elib:https://elib.dlr.de/112615/
Document Type:Conference or Workshop Item (Speech)
Title:A Record Flight of the Hybrid Sounding Rocket HEROS 3
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Kobald, MarioMario.Kobald (at) dlr.dehttps://orcid.org/0000-0002-1708-3944
Schmierer, C.christian.schmierer (at) dlr.deUNSPECIFIED
Fischer, U.ulrich.fischer (at) dlr.deUNSPECIFIED
Tomilin, K.konstantin.tomilin (at) dlr.deUNSPECIFIED
Petrarolo, Annaanna.petrarolo (at) dlr.dehttps://orcid.org/0000-0002-2291-2874
Date:6 June 2017
Refereed publication:Yes
Open Access:No
In DOAJ:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Hybrid rocket Propulsion, sounding rocket, Paraffin fuel, nitrous oxide, world record
Event Title:31st International Symposium on Space Technology and Science (ISTS)
Event Location:Matsuyama, Japan
Event Type:international Conference
Event Dates:3.-9. Jun. 2017
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 - Wiederverwendbare Raumfahrtsysteme und Antriebstechnologie
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Treibstoffe
Deposited By: Kobald, Dr. Mario
Deposited On:09 Jun 2017 08:42
Last Modified:01 Dec 2018 19:52

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