Paper
13 June 2007 Performance testing of a large heat lift 40 to 80K pulse tube cooler for space applications
T. Trollier, J. Tanchon, J. Buquet, G. Aigouy, A. Ravex, I. Charles, A. Coynel, L. Duband, E. Ercolani, L. Guillemet, J. Mullié, T. Benschop, M. Linder
Author Affiliations +
Abstract
A Large heat lift 40 to 80K Pulse Tube Cooler (LPTC) has been designed, manufactured and tested in partnership between AL/DTA, CEA/SBT and THALES Cryogenics BV. The Engineering Model specification of 2.3 W cooling power at 50 K for 10°C rejection temperature and maximum 160 watts electrical input power has been reached. The as built model weighs 5.13 kg. The thermal and mechanical performances are presented and discussed. This work is funded by the European Space Agency (ESA/ESTEC Contract N°18433/04/NL/AR) in the frame of future Earth Observation instruments development.
© (2007) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
T. Trollier, J. Tanchon, J. Buquet, G. Aigouy, A. Ravex, I. Charles, A. Coynel, L. Duband, E. Ercolani, L. Guillemet, J. Mullié, T. Benschop, and M. Linder "Performance testing of a large heat lift 40 to 80K pulse tube cooler for space applications", Proc. SPIE 6542, Infrared Technology and Applications XXXIII, 65422K (13 June 2007); https://doi.org/10.1117/12.721514
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Cited by 6 scholarly publications.
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KEYWORDS
Sensors

Interfaces

Computer aided design

Temperature metrology

Cryogenics

Manufacturing

Design for manufacturability

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