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ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering Conference - CEC | 2014

Pulse tube coolers for Meteosat third generation

James Butterworth; Gérald Aigouy; Clement Chassaing; Benoı̂t Debray; Alexandre Huguet

Air Liquides Large Pulse Tube Coolers (LPTC) will be used to cool the focal planes of the Infrared Sounder (IRS) and Flexible Combined Imager (FCI) instruments aboard the ESA/Eumetsat satellites Meteosat Third Generation (MTG). This cooler consists of an opposed piston linear compressor driving a pulse tube cold head and the associated drive electronics including temperature regulation and vibration cancellation algorithms. Preparations for flight qualification of the cooler are now underway. In this paper we present results of the optimization and qualification activities as well as an update on endurance testing.


ADVANCES IN CRYOGENIC ENGINEERING: Transactions of the Cryogenic Engineering Conference - CEC | 2014

150K - 200K miniature pulse tube cooler for micro satellites

Clement Chassaing; James Butterworth; Gérald Aigouy; Christophe Daniel; Maurice Crespin; Eric Duvivier

Air Liquide is working with the CNES and Steel electronique in 2013 to design, manufacture and test a Miniature Pulse Tube Cooler (MPTC) to cool infrared detectors for micro-satellite missions. The cooler will be particularly adapted to the needs of the CNES MICROCARB mission to study atmospheric Carbon Dioxide which presents absorption lines in the thermal near infrared, at 1.6 μm and 2.0 μm. The required cooler temperature is from 150 to 200K with cooling power between 1 and 3 watts. The overall electrical power budget including electronics is less than 20W with a 288-300K rejection temperature. Particular attention is therefore paid to optimizing overall system efficiency. The active micro vibration reduction system and thermal control systems already developed for the Air Liquide Large Pulse Tube Cooler (LPTC) are currently being implemented into a new high efficiency electronic architecture. The presented work concerns the new cold finger and electronic design. The cooler uses the compressor already developed for the 80K Miniature Pulse Tube Cryocooler. This Pulse Tube Cooler addresses the requirements of space missions where extended continuous operating life time (>5 years), low mass and low micro vibration levels are critical.


Archive | 2011

Method and Equipment for Pulsed Charge Refrigeration

Gérald Aigouy; Jean-Marc Bernhardt; Pierre Briend; Eric Fauve; David Grillot; Vincent Heloin


Archive | 2011

Refrigeration method and apparatus with a pulsating load

Gérald Aigouy; Pierre Briend; Cindy Deschildre; Eric Fauve; Jean-Marc Bernhardt; Franck Delcayre


Archive | 2012

Linear Electrodynamic-Type Motor, Cryocooler Including Such a Motor and Method Implementing Such a Motor

Gérald Aigouy; James Butterworth; Benoît Debray; Jean Christophe Rey


Archive | 2013

Dispositif et procédé de remplissage de réservoir

Gérald Aigouy; James Butterworth


Archive | 2013

Tank filling device and method

Gérald Aigouy; James Butterworth


Archive | 2016

Method and equipment for pulsed charge cooling of a component of a tokomak

Gérald Aigouy; Jean-Marc Bernhardt; Pierre Briend; Eric Fauve; David Grillot; Vincent Heloin


Archive | 2015

A cryogenic refrigeration

James Butterworth; Gérald Aigouy; Sylvain Martin; Clement Chassaing


Archive | 2012

Device and process to damp parasitic loads in a linear electrodynamic motor and linear electrodynamic motor comprising such a device

Gérald Aigouy; Benoît Debray; Jean-Christophe Rey

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