This paper describes the experimental characterization of an auto-lubricating vane pump (Gardner Denver Thomas G 24/04 EB) in simulated Mars environment. The pump volumetric flow rate has been measured upon varying the pressure difference between the intake and the discharge. Tests have been performed with a measurement system designed to operate both in terrestrial atmospheric conditions and in controlled pressure and temperature conditions. No degradation between the pump behavior in Mars pressure and in normal atmospheric pressure was detected. The pump has been eventually redesigned in order to assure resistance against mechanical loading at launch and landing and using materials compatible withthe space and Mars environment. © 2014 IEEE.

Characterization of a pumping system in Martian-like environment

Saggin B.;
2014

Abstract

This paper describes the experimental characterization of an auto-lubricating vane pump (Gardner Denver Thomas G 24/04 EB) in simulated Mars environment. The pump volumetric flow rate has been measured upon varying the pressure difference between the intake and the discharge. Tests have been performed with a measurement system designed to operate both in terrestrial atmospheric conditions and in controlled pressure and temperature conditions. No degradation between the pump behavior in Mars pressure and in normal atmospheric pressure was detected. The pump has been eventually redesigned in order to assure resistance against mechanical loading at launch and landing and using materials compatible withthe space and Mars environment. © 2014 IEEE.
2014
2014 IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2014 - Proceedings
2014 IEEE International Workshop on Metrology for Aerospace, MetroAeroSpace 2014
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11577/3523637
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