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Fischer, U. (2016) Design, Integration und Test einer fortschrittlichen Hybrid-Höhenforschungsrakete auf Basis von Leichtbauwerkstoffen Design, Assembly and Test of an Advanced Hybrid-sounding Rocket based on Light-weight Materials. DLR-Interner Bericht. DLR-IB-RA-LA-2016-251. Diploma. Universität Stuttgart. 88 S.
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Abstract
An experimental rocket, using a hybrid rocket engine, developed by the student group HyEnD (Hybrid Engine Development) is designed to reach an altitude of over 20 kilometers. Two rockets have been built during the project. The rocket MIRAS (MIcro RAkete Stuttgart) is a technology demonstrator used to gain experience in manufacturing and operating hybrid rockets. In parallel the HEROS (Hybrid Experimental ROcket Stuttgart) rocket is developed. It is designed to reach the mission objectives required in the STERN project. The design, calculation und manufacturing of the HEROS rockets structural elements, using fiber reinforced plastic, is subject of this thesis. The application of integral structure components in the design of fins and the oxidizer tank is investigated. Cost efficient manufacturing methods of fiber reinforced plastic regarding to prototype construction is described. A flight test is conducted to evaluate the rockets design.
| Item URL in elib: | https://elib.dlr.de/107824/ | ||||||
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| Document Type: | Monograph (DLR-Interner Bericht, Diploma) | ||||||
| Title: | Design, Integration und Test einer fortschrittlichen Hybrid-Höhenforschungsrakete auf Basis von Leichtbauwerkstoffen Design, Assembly and Test of an Advanced Hybrid-sounding Rocket based on Light-weight Materials | ||||||
| Authors: |
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| Date: | 2016 | ||||||
| Refereed publication: | No | ||||||
| Open Access: | No | ||||||
| Gold Open Access: | No | ||||||
| In SCOPUS: | No | ||||||
| In ISI Web of Science: | No | ||||||
| Number of Pages: | 88 | ||||||
| Status: | Published | ||||||
| Keywords: | hybrid rocket, CFRP, structure, flight test, prototype manifacturing | ||||||
| Institution: | Universität Stuttgart | ||||||
| Department: | Institut für Raumfahrtsysteme | ||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||
| HGF - Program: | Space | ||||||
| HGF - Program Themes: | Space Transportation | ||||||
| DLR - Research area: | Raumfahrt | ||||||
| DLR - Program: | R KN - Kommunikation und Navigation | ||||||
| DLR - Research theme (Project): | R - Projekt Treibstoffe (old) | ||||||
| Location: | Lampoldshausen | ||||||
| Institutes and Institutions: | Institute of Space Propulsion > Propellants | ||||||
| Deposited By: | Schmidt, Melanie | ||||||
| Deposited On: | 16 Nov 2016 07:57 | ||||||
| Last Modified: | 16 Nov 2016 07:57 |
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