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Modelling and experimental validation of the heat accumulator in a Low Trust Cryogenic Propulsion (LTCP) system¿¿e,

Autor
Torras, S.; Castro, J.; Rigola, J.; Morales, S.; Riccius, J.; Leiner, J.
Tipus d'activitat
Presentació treball a congrés
Nom de l'edició
5th European Conference for Aeronautics and Space Sciences
Any de l'edició
2013
Data de presentació
2013-07-02
Llibre d'actes
Proceedings of 5th European Conference for Aeronautics an Space Sciences (EUCASS)
Pàgina inicial
1
Pàgina final
15
Repositori
http://hdl.handle.net/2117/105100 Obrir en finestra nova
Resum
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 ...
Citació
Torras, S., Castro, J., Rigola, J., Morales, S., Riccius, J., Leiner, J. Modelling and experimental validation of the heat accumulator in a Low Trust Cryogenic Propulsion (LTCP) system¿¿e,. A: European Conference for Aerospace Sciences. "Proceedings of 5th European Conference for Aeronautics an Space Sciences (EUCASS)". Munich: 2013, p. 1-15.
Grup de recerca
CTTC - Centre Tecnològic de la Transferència de Calor

Participants