Kobald, Mario und Ciezki, Helmut und Schlechtriem, S. und Toson, E. (2013) Rheological, Optical And Ballistic Investigations Of Paraffin-Based Fuels For Hybrid Rocket Propulsion Using a 2D Slab-Burner. In: Proceedings 5th EUCASS. 5th European Conference for Aeronautics and Space Sciences EUCASS 2013, 1. - 5. Jul. 2013, München, Germany. ISBN 978-84-941531-0-5.
Es ist eine neuere Version dieses Eintrags verfügbar. |
Dieses Archiv kann nicht den Volltext zur Verfügung stellen.
Kurzfassung
This paper describes combined rheological, ballistic and optical analyses performed on paran-based mixtures that can be used as high regression rate hybrid rocket fuels. Experimental activities have been done at the DLR Institute of Space Propulsion in Lampoldshausen and at Space Propulsion Laboratory (SPLab) of Politecnico di Milano [1]. This paper describes in detail the experiments performed at the DLR. Viscosity, surface tension and regression rate of the fuels have been determined. Furthermore the combustion was evaluated by optical measurements. Data collected so far indicates an increasing regression rate for decreasing viscosity of the liquid paran.
elib-URL des Eintrags: | https://elib.dlr.de/85321/ | ||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
Titel: | Rheological, Optical And Ballistic Investigations Of Paraffin-Based Fuels For Hybrid Rocket Propulsion Using a 2D Slab-Burner | ||||||||||||||||||||
Autoren: |
| ||||||||||||||||||||
Datum: | 2013 | ||||||||||||||||||||
Erschienen in: | Proceedings 5th EUCASS | ||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||
ISBN: | 978-84-941531-0-5 | ||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | hybrid rocket fuels, rheological | ||||||||||||||||||||
Veranstaltungstitel: | 5th European Conference for Aeronautics and Space Sciences EUCASS 2013 | ||||||||||||||||||||
Veranstaltungsort: | München, Germany | ||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
Veranstaltungsdatum: | 1. - 5. Jul. 2013 | ||||||||||||||||||||
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 - Schubkammertechnologie (alt) | ||||||||||||||||||||
Standort: | Lampoldshausen | ||||||||||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe > Treibstoffe | ||||||||||||||||||||
Hinterlegt von: | Hanke, Michaela | ||||||||||||||||||||
Hinterlegt am: | 22 Nov 2013 08:53 | ||||||||||||||||||||
Letzte Änderung: | 29 Mär 2023 00:18 |
Verfügbare Versionen dieses Eintrags
-
Ignition Delay Times of Kerosene (Jet-A)/Air Mixtures. (deposited 11 Nov 2013 08:46)
-
Numerical Simulations of Flame of Single Co-Axial Injector. (deposited 22 Nov 2013 09:20)
-
Wall Heat Fluxes in Rocket Combustion Chamber with Porous Injector Head. (deposited 22 Nov 2013 09:06)
-
Modelling Acoustic Excitation of High Frequency Combustion Instability Experiments. (deposited 22 Nov 2013 09:27)
-
A Prediction of Methodology for the High Cycle Fatigue Life of Hydrogen-Loaded Structures. (deposited 22 Nov 2013 09:05)
-
Rheological and ballistic investigations of paraffin-based fuels for hybrid rocket propulsion using a 2D radial micro-burner. (deposited 22 Nov 2013 09:09)
- Rheological, Optical And Ballistic Investigations Of Paraffin-Based Fuels For Hybrid Rocket Propulsion Using a 2D Slab-Burner. (deposited 22 Nov 2013 08:53) [Gegenwärtig angezeigt]
-
Rheological and ballistic investigations of paraffin-based fuels for hybrid rocket propulsion using a 2D radial micro-burner. (deposited 22 Nov 2013 09:09)
-
A Prediction of Methodology for the High Cycle Fatigue Life of Hydrogen-Loaded Structures. (deposited 22 Nov 2013 09:05)
- Experimental Investigation of Acoustic Energy Dissipation in a Rectangular Combustion Chamber. (deposited 22 Nov 2013 09:07)
-
Stability behaviour of a cylindrical rocket engine combustion chamber operated with liquid hydrogen and liquid oxygen. (deposited 22 Nov 2013 09:01)
-
Cryogenic oxygen jet response to transverse acoustic
excitation with 1T and 1L1T modes. (deposited 22 Nov 2013 09:19)
-
Heat transfer in porous media applied to liquid rocket engines. (deposited 22 Nov 2013 09:01)
-
Student Hybrid Thruster Testing and Research. (deposited 22 Nov 2013 09:12)
-
Modelling and experimental validation of the heat accumulator in a Low Trust Cryogenic Propulsion (LTCP) system. (deposited 22 Nov 2013 09:00)
- Characterization of a double swirl injector in a LOX/LCH4 fueled combustor on Mascotte test bench. (deposited 22 Nov 2013 09:11)
-
Modelling and experimental validation of the heat accumulator in a Low Trust Cryogenic Propulsion (LTCP) system. (deposited 22 Nov 2013 09:00)
-
Student Hybrid Thruster Testing and Research. (deposited 22 Nov 2013 09:12)
-
Heat transfer in porous media applied to liquid rocket engines. (deposited 22 Nov 2013 09:01)
-
Cryogenic oxygen jet response to transverse acoustic
excitation with 1T and 1L1T modes. (deposited 22 Nov 2013 09:19)
-
Modelling Acoustic Excitation of High Frequency Combustion Instability Experiments. (deposited 22 Nov 2013 09:27)
- Flow Separation in Out-of-Round Nozzles, a Numerical and Experimental Study. (deposited 22 Nov 2013 09:02)
-
Wall Heat Fluxes in Rocket Combustion Chamber with Porous Injector Head. (deposited 22 Nov 2013 09:06)
-
Numerical Simulations of Flame of Single Co-Axial Injector. (deposited 22 Nov 2013 09:20)
Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags