Riccius, Jörg und Leiner, J. und Torras, S. und Rigola, J. und Morales, S. (2013) Modelling and experimental validation of the heat accumulator in a Low Trust Cryogenic Propulsion (LTCP) system. 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
The study of one of the components, the heat accumulator, of Low Thrust Cryogenic Propulsion systems (LTCP), is of scientific interest in the framework of ISP-1 project [1]. This device stores thermal energy from the fuel cell that provides electrical energy to the whole system. This thermal energy is employed for the pressurization of the propellant tanks. A numerical model is being developed [2] in order to predict the thermal behaviour of the heat accumulator and having a tool for its design in the next future. The numerical model is validated with experimental results of ISP-1 partners (DLR) [3], [4].
elib-URL des Eintrags: | https://elib.dlr.de/85316/ | ||||||||||||||||||||||||
---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||
Titel: | Modelling and experimental validation of the heat accumulator in a Low Trust Cryogenic Propulsion (LTCP) system | ||||||||||||||||||||||||
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: | heat accumulator, cryogenic propulsion | ||||||||||||||||||||||||
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 > Raketenantriebe | ||||||||||||||||||||||||
Hinterlegt von: | Hanke, Michaela | ||||||||||||||||||||||||
Hinterlegt am: | 22 Nov 2013 09:00 | ||||||||||||||||||||||||
Letzte Änderung: | 01 Dez 2018 19:49 |
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)
- 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)
[Gegenwärtig angezeigt]
- 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)
[Gegenwärtig angezeigt]
-
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)
- 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