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Hot run test results of a validation optimized water-ice phase change heat accumulator and comparison to numerical analysis¿X¿¿c

Author
Riccius, J.; Leiner, J.; Castro, J.; Rigola, J.
Type of activity
Presentation of work at congresses
Name of edition
5th European Conference for Aeronautics and Space Sciences
Date of publication
2013
Presentation's date
2013-07-02
Book of congress proceedings
Proceedings of 5th European Conference for Aeronautics an Space Sciences (EUCASS)
First page
1
Last page
12
Repository
http://hdl.handle.net/2117/105102 Open in new window
Abstract
Phase change heat accumulators are essential devices for the thermal management of multiple ignition, electric pump driven in-space propulsion systems such as the Low Cost Cryogenic Propulsion (LCCP) system [1], [2]. For Low Temperature Accumulators (LTAs), water/ice is of special interest as phase change material because of its high heat capacity and high latent heat. Therefore, an analysis of the phase change behaviour of both, this heat storage material and an heat transfer medium were perfor...
Citation
Riccius, J., Leiner, J., Castro, J., Rigola, J. Hot run test results of a validation optimized water-ice phase change heat accumulator and comparison to numerical analysis¿X¿¿c. A: European Conference for Aerospace Sciences. "Proceedings of 5th European Conference for Aeronautics an Space Sciences (EUCASS)". Munich: 2013, p. 1-12.
Group of research
CTTC - Heat and Mass Transfer Technological Center

Participants