van Kleef, Arnaud und Oving, Bertil und Verberne, C. J. und Haemmerli, Bastien und Kuhn, Markus und Müller, Ilja und Petkov, Ivaylo (2015) Innovative Small Launcher. Springer. 13th Reinventing Space Conference, 09.-13. Nov. 2015, Oxford, Großbritannien. doi: 10.1007/978-3-319-32817-1_7. ISBN 978-3-319-32817-1.
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Offizielle URL: https://doi.org/10.1007/978-3-319-32817-1_7
Kurzfassung
The market for small satellites is expected to increase substantially in the coming years, but there is little capacity to launch them affordably. No operational dedicated launcher for small satellites exists today. Small satellites, launched as secondary payloads, are entirely dependent on the constraints set by the primary payload, such as launch date and target orbit. Launch costs of less than €50,000 per kg of payload are required in order to directly compete with piggy-back ride shares. With a dedicated launcher a higher cost per kg can be accepted for payloads which need to be delivered timely and accurately to a desired orbit. --- A consortium of 13 companies and institutes are joining forces in a Horizon 2020 work programme to design a dedicated small launcher to be built in and launched from Europe. The project is called SMall Innovative Launcher for Europe (SMILE) starting in 2016. The SMILE project aims at a combined research approach into a new innovative European launcher for an emerging market of small satellites up to 50 kg using a multidisciplinary design and optimisation approach strengthened by the demonstration of critical technologies for cost-effective solutions and complemented with the design of a European-based launch capability from Andøya (Norway). For the intended market, cost reduction is essential. One option to reduce cost is to apply reusability of one or more of the stages. Cost can also be reduced by applying commercial industry-grade components. Another means of cost reduction is through volume production. Finally, the production process can be optimized for cost, e.g. automated manufacturing for composite parts and 3D-printing for metallic parts. Critical launcher technologies in various expertise areas will be developed in SMILE, but this paper focusses on the rocket engine developments and their impact on cost reduction and design since the engines are the most critical and expensive parts of a launcher. For the rocket propulsion system, both hybrid engines and reusable liquid engines are assessed.
elib-URL des Eintrags: | https://elib.dlr.de/120237/ | ||||||||||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||||||
Zusätzliche Informationen: | Conference No. BIS-RS-2015-16 | ||||||||||||||||||||||||||||||||
Titel: | Innovative Small Launcher | ||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | 11 November 2015 | ||||||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||||||
DOI: | 10.1007/978-3-319-32817-1_7 | ||||||||||||||||||||||||||||||||
Seitenbereich: | Seiten 59-16 | ||||||||||||||||||||||||||||||||
Herausgeber: |
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Verlag: | Springer | ||||||||||||||||||||||||||||||||
Name der Reihe: | Proceedings of the 13th Reinventing Space Conference | ||||||||||||||||||||||||||||||||
ISBN: | 978-3-319-32817-1 | ||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||
Stichwörter: | Cost-Effective Launcher, Hybrid Rocket Propulsion, Innovative Propulsion Concepts, LPRE, Liquid Rocket Propulsion, Microlauncher, SMILE | ||||||||||||||||||||||||||||||||
Veranstaltungstitel: | 13th Reinventing Space Conference | ||||||||||||||||||||||||||||||||
Veranstaltungsort: | Oxford, Großbritannien | ||||||||||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||||||
Veranstaltungsdatum: | 09.-13. Nov. 2015 | ||||||||||||||||||||||||||||||||
Veranstalter : | British Interplanetary Society | ||||||||||||||||||||||||||||||||
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 - EU Projekte Raumtransport (alt), R - Antriebsystemtechnik - Schubkammertechnologie (alt) | ||||||||||||||||||||||||||||||||
Standort: | Stuttgart | ||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Bauweisen und Strukturtechnologie > Raumfahrt - System - Integration | ||||||||||||||||||||||||||||||||
Hinterlegt von: | Kuhn, Markus | ||||||||||||||||||||||||||||||||
Hinterlegt am: | 14 Jun 2018 15:44 | ||||||||||||||||||||||||||||||||
Letzte Änderung: | 20 Jun 2021 15:51 |
Verfügbare Versionen dieses Eintrags
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Innovative Small Launcher. (deposited 13 Jan 2016 12:13)
- Innovative Small Launcher. (deposited 14 Jun 2018 15:44) [Gegenwärtig angezeigt]
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