Kobald, Mario und Fischer, U. und Tomilin, K. und Schmierer, C. und Petrarolo, Anna (2017) Hybrid Sounding Rocket HEROS TRL 9. 7th European Conference for Aeronautics and Space Sciences (EUCASS), 2017-07-03 - 2017-07-06, Mailand, Italien.
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Kurzfassung
The inherent safety of hybrid rocket propulsion offers some unique advantages compared to solid and liquid propellant rocket engines. This makes it especially attractive for space tourism, Micro-launcher and hands-on experiments in the education of students. 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 and a world altitude record for hybrid rockets built by students. The 7.5m long rocket is using Nitrous Oxide (N2O) and a Paraffin-based fuel to produce 10,000 N of thrust. The dry mass of the rocket was only 75 kg thanks to a carbon fibre structure for the most part. The rocket performed the record breaking flight at perfect weather and visibility conditions, reaching a maximum airspeed of 720 m/s and Mach 2.3. The rocket performed a soft landing with two parachutes and can be reused. Flight data and engine performance data are published and analyzed. The flight data shows excellent stability of the rocket. Engine performance data proves very high efficiency and stable combustion as in the ground tests. Engine and flight trajectory simulations show very good agreements with the flight data. Furthermore, the overall project, the rockets design as well as the launch campaign are presented here in detail.
elib-URL des Eintrags: | https://elib.dlr.de/113124/ | ||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||
Titel: | Hybrid Sounding Rocket HEROS TRL 9 | ||||||||||||||||||||||||
Autoren: |
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Datum: | 3 Juli 2017 | ||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Stichwörter: | Hybrid rocket Propulsion, Sounding Rocket, Altitude Record, Paraffin fuel, nitrous oxide | ||||||||||||||||||||||||
Veranstaltungstitel: | 7th European Conference for Aeronautics and Space Sciences (EUCASS) | ||||||||||||||||||||||||
Veranstaltungsort: | Mailand, Italien | ||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||
Veranstaltungsbeginn: | 3 Juli 2017 | ||||||||||||||||||||||||
Veranstaltungsende: | 6 Juli 2017 | ||||||||||||||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||||||||||||||
HGF - Programmthema: | Raumtransport | ||||||||||||||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||||||||||
DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Antriebsystemtechnik - Raketenantriebtests (alt) | ||||||||||||||||||||||||
Standort: | Lampoldshausen | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe | ||||||||||||||||||||||||
Hinterlegt von: | Kobald, Dr. Mario | ||||||||||||||||||||||||
Hinterlegt am: | 07 Jul 2017 08:52 | ||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:17 |
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