TY - JOUR
T1 - Graphene loop heat pipe in space
AU - Molina, Marco
AU - Pilato, Giuseppe
AU - Palermo, Vincenzo
AU - Christian, Meganne
AU - Morandi, Vittorio
AU - Iorio, Carlo S.
AU - Queeckers, Patrick
AU - Ferrara, Andrea
AU - Iermano, Fabio
AU - Lombardi, Lucia
AU - Minetti, Christophe
AU - Papakinstantinou, Constantine
AU - Samad, Yarjan A.
AU - Ferrari, Andrea C.
N1 - Funding Information:
The research leading to these results has received funding from the European Union H2020 Programme under Grant agreement number 785219: Graphene Flagship.
Publisher Copyright:
Copyright © 2018 by Leonardo Spa. Published by the IAF, with permission and released to the IAF to publish in all forms. All right reserved.
PY - 2018
Y1 - 2018
N2 - We report a graphene enhanced capillary pump for a Loop Heat Pipe (LHP). LHPs are passive devices for thermal control of equipment and payloads for satellites and probes. Capable to transfer heat from sources to the satellite radiators, LHPs use the waste heat of the devices to be cooled as the driving energy for pumping a fluid through a loop. The core of a LHP is a capillary pump, a phase separator that allows pressure being generated by capillarity across a porous structure, in two-phase conditions for the operating fluid. Traditionally, LHPs capillary pumps are sintered metallic wicks. Various properties of graphene have been considered for enhancing the LHP performance, acting at capillary pump level: porosity, wettability and thermal conductivity. Major issues in using conventional LHPs, i.e. with metallic wicks, in operational space missions are related to their non-deterministic start-up behaviour. Additionally, reliable LHPs are required to ensure operations without interruption for the entire mission duration. Superior start-up capabilities have been achieved with graphene oxide coated Ni sintered wicks, using acetone as a fluid, operated in a vacuum chamber on ground. A LHP capillary pump was tested during a zero-g parabolic flights campaign, to eliminate gravity effects. The measurements show up to 8 times improvement in evaporation rate compared a conventional metal only wick.
AB - We report a graphene enhanced capillary pump for a Loop Heat Pipe (LHP). LHPs are passive devices for thermal control of equipment and payloads for satellites and probes. Capable to transfer heat from sources to the satellite radiators, LHPs use the waste heat of the devices to be cooled as the driving energy for pumping a fluid through a loop. The core of a LHP is a capillary pump, a phase separator that allows pressure being generated by capillarity across a porous structure, in two-phase conditions for the operating fluid. Traditionally, LHPs capillary pumps are sintered metallic wicks. Various properties of graphene have been considered for enhancing the LHP performance, acting at capillary pump level: porosity, wettability and thermal conductivity. Major issues in using conventional LHPs, i.e. with metallic wicks, in operational space missions are related to their non-deterministic start-up behaviour. Additionally, reliable LHPs are required to ensure operations without interruption for the entire mission duration. Superior start-up capabilities have been achieved with graphene oxide coated Ni sintered wicks, using acetone as a fluid, operated in a vacuum chamber on ground. A LHP capillary pump was tested during a zero-g parabolic flights campaign, to eliminate gravity effects. The measurements show up to 8 times improvement in evaporation rate compared a conventional metal only wick.
KW - Graphene
KW - Loop Heat Pipe
KW - Space Equipment
UR - http://www.scopus.com/inward/record.url?scp=85065290349&partnerID=8YFLogxK
M3 - Conference article
AN - SCOPUS:85065290349
SN - 0074-1795
VL - 2018-October
JO - Proceedings of the International Astronautical Congress, IAC
JF - Proceedings of the International Astronautical Congress, IAC
T2 - 69th International Astronautical Congress: #InvolvingEveryone, IAC 2018
Y2 - 1 October 2018 through 5 October 2018
ER -