Numerical modelling of the phase change material heat accumulator under fast transient gasification conditions in a low thrust cryogenic propulsion (LTCP) system

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To access the full text documents, please follow this link: http://hdl.handle.net/2117/109333

dc.contributor	Universitat Politècnica de Catalunya. Departament de Màquines i Motors Tèrmics
dc.contributor	Universitat Politècnica de Catalunya. CTTC - Centre Tecnològic de la Transferència de Calor
dc.contributor.author	Castro González, Jesús
dc.contributor.author	Galione Klot, Pedro Andrés
dc.contributor.author	Morales Ruiz, Juan José
dc.contributor.author	Lehmkuhl Barba, Oriol
dc.contributor.author	Rigola Serrano, Joaquim
dc.contributor.author	Pérez Segarra, Carlos David
dc.contributor.author	Oliva Llena, Asensio
dc.date	2012
dc.identifier.citation	Castro, J., Galione, P.A., Morales, J., Lehmkuhl, O., Rigola, J., Perez, C., Oliva, A. "Numerical modelling of the phase change material heat accumulator under fast transient gasification conditions in a low thrust cryogenic propulsion (LTCP) system". Bordeaux: 2012.
dc.identifier.uri	http://hdl.handle.net/2117/109333
dc.language.iso	eng
dc.relation	http://cataleg.upc.edu/record=b1420732~S1*cat
dc.rights	info:eu-repo/semantics/openAccess
dc.subject	Àrees temàtiques de la UPC::Energies::Tecnologia energètica
dc.subject	Storage batteries
dc.subject	Propulsion systems
dc.subject	Acumuladors
dc.subject	Sistemes de propulsió
dc.title	Numerical modelling of the phase change material heat accumulator under fast transient gasification conditions in a low thrust cryogenic propulsion (LTCP) system
dc.type	info:eu-repo/semantics/publishedVersion
dc.type	info:eu-repo/semantics/report
dc.description.abstract	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. Two different types of heat accumulators are present in the LTCP system: the High Temperature Accumulator (HTA) and the Low Temperature Accumulator (LTA). A numerical model is being developed [2] in order to predict the thermal behavior of the LTA and having a tool for its design in the next future. Experimental results of ISP-1 partners of DLR are being used for the validation [3], [4].

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