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Conception of a compact flow boiling loop for the International Space Station- First results in parabolic flights

Authors :
Paul Chorin
Antoine Boned
Julien Sebilleau
Catherine Colin
Olaf Schoele-Schulz
Nicola Picchi
Christian Schwarz
Balazs Toth
Daniele Mangini
Institut de mécanique des fluides de Toulouse (IMFT)
Université Toulouse III - Paul Sabatier (UT3)
Université de Toulouse (UT)-Université de Toulouse (UT)-Centre National de la Recherche Scientifique (CNRS)-Institut National Polytechnique (Toulouse) (Toulouse INP)
Université de Toulouse (UT)
Fédération de Recherche Fluides, Energie, Réacteurs, Matériaux et Transferts (FERMAT)
Institut National des Sciences Appliquées - Toulouse (INSA Toulouse)
Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Institut National des Sciences Appliquées (INSA)-Université de Toulouse (UT)-Université Toulouse III - Paul Sabatier (UT3)
Université de Toulouse (UT)-Centre National de la Recherche Scientifique (CNRS)-Institut National Polytechnique (Toulouse) (Toulouse INP)
Airbus Defence and Space [Bremen]
Airbus Defence and Space [Taufkirchen]
European Space Research and Technology Centre (ESTEC)
Agence Spatiale Européenne = European Space Agency (ESA)
GDR 2799 Micropesanteur Fondamentale & Appliquée
Source :
Comptes Rendus. Mécanique, Comptes Rendus. Mécanique, 2023, 351 (S2), pp.1-20. ⟨10.5802/crmeca.147⟩
Publication Year :
2023
Publisher :
Cellule MathDoc/CEDRAM, 2023.

Abstract

International audience; The design of a pipe flow boiling experiment for the International Space Station is proposed, taking into account typical weight, power consumption and size constraints. The effect of singularities such as elbows upstream the test section is investigated. Velocity profiles downstream two elbows, measured by Particle Image Velocimetry are in good agreement with numerical simulation and allow to determine a specific distance (decay length) downstream the elbows for which the velocity profile recover its axisymmetry. From these results a breadboard is designed and tested in parabolic flights. Care has been taken to generate boiling downstream the decay length. Two-phase bubbly flow is observed with 2 perpendicular high-speed cameras in the test section and a symmetry of the bubble distribution in the pipe is verified for different gravity conditions when the bubbles are created after the decay length.

Details

ISSN :
18737234 and 16310721
Volume :
351
Database :
OpenAIRE
Journal :
Comptes Rendus. Mécanique
Accession number :
edsair.doi.dedup.....8c68ebcb77114e50bfd534ff5ef85219