Design of a large heat lift 40 K to 80 K pulse tube cryocooler for space applications

T. Trollier; J. Tanchon; J. Buquet; A. Ravex; I. Charles; A. Coynel; L. Duband; E. Ercolani; L. Guillemet; J. Mullié; J.A.M. Dam; T. Benschop; M. Linder

Design of a large heat lift 40 K to 80 K pulse tube cryocooler for space applications

T. Trollier, J. Tanchon, J. Buquet, A. Ravex, I. Charles, A. Coynel, L. Duband, E. Ercolani, L. Guillemet, J. Mullié, J.A.M. Dam, T. Benschop, M. Linder

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

Abstract

A Large heat lift Pulse Tube Cooler (LPTC) is under development in partnership with AL/ DTA, CEA/SBT and THALES Cryogenics. The engineering model is expected to provide 2.3 W at 50 K at a 10 °C rejection temperature and 160 watts of electrical input power to the compressor. The split coaxial design of the pulse tube cold finger and the moving magnet linear motor compressor design will be presented. The expected thermal and mechanical performances will be also discussed. The engineering model will be delivered to ESA/ESTEC in October 2006 after completion of a qualification test program. This work is funded by the European Space Agency (ESA/ESTEC Contract N° 8433/04/NL/AR) for future earth observation instrument missions.

Original language	English
Title of host publication	Proceedings of the 14th International Cryocooler Conference (ICC 14) 14-16 June 2006, Annapolis, Maryland, USA
Editors	S.D. Miller, R.G. Ross, Jr.
Place of Publication	Boulder CO
Publisher	ICC Press
Pages	75-82
ISBN (Print)	978-1-934021-00-2
Publication status	Published - 2007
Event	14th International Cryocooler Conference (Cryocoolers 14), June 14-16, 2006, Annapolis, MD, USA - Annapolis, MD, United States Duration: 14 Jun 2006 → 16 Jun 2006

Conference

Conference	14th International Cryocooler Conference (Cryocoolers 14), June 14-16, 2006, Annapolis, MD, USA
Abbreviated title	Cryocoolers 14
Country/Territory	United States
City	Annapolis, MD
Period	14/06/06 → 16/06/06

Cite this

Trollier, T., Tanchon, J., Buquet, J., Ravex, A., Charles, I., Coynel, A., Duband, L., Ercolani, E., Guillemet, L., Mullié, J., Dam, J. A. M., Benschop, T., & Linder, M. (2007). Design of a large heat lift 40 K to 80 K pulse tube cryocooler for space applications. In S. D. Miller, & R. G. Ross, Jr. (Eds.), Proceedings of the 14th International Cryocooler Conference (ICC 14) 14-16 June 2006, Annapolis, Maryland, USA (pp. 75-82). ICC Press.

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title = "Design of a large heat lift 40 K to 80 K pulse tube cryocooler for space applications",

abstract = "A Large heat lift Pulse Tube Cooler (LPTC) is under development in partnership with AL/ DTA, CEA/SBT and THALES Cryogenics. The engineering model is expected to provide 2.3 W at 50 K at a 10 °C rejection temperature and 160 watts of electrical input power to the compressor. The split coaxial design of the pulse tube cold finger and the moving magnet linear motor compressor design will be presented. The expected thermal and mechanical performances will be also discussed. The engineering model will be delivered to ESA/ESTEC in October 2006 after completion of a qualification test program. This work is funded by the European Space Agency (ESA/ESTEC Contract N° 8433/04/NL/AR) for future earth observation instrument missions.",

author = "T. Trollier and J. Tanchon and J. Buquet and A. Ravex and I. Charles and A. Coynel and L. Duband and E. Ercolani and L. Guillemet and J. Mulli{\'e} and J.A.M. Dam and T. Benschop and M. Linder",

year = "2007",

language = "English",

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pages = "75--82",

editor = "S.D. Miller and {Ross, Jr.}, R.G.",

booktitle = "Proceedings of the 14th International Cryocooler Conference (ICC 14) 14-16 June 2006, Annapolis, Maryland, USA",

publisher = "ICC Press",

note = "14th International Cryocooler Conference (Cryocoolers 14), June 14-16, 2006, Annapolis, MD, USA, Cryocoolers 14 ; Conference date: 14-06-2006 Through 16-06-2006",

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Trollier, T, Tanchon, J, Buquet, J, Ravex, A, Charles, I, Coynel, A, Duband, L, Ercolani, E, Guillemet, L, Mullié, J, Dam, JAM, Benschop, T & Linder, M 2007, Design of a large heat lift 40 K to 80 K pulse tube cryocooler for space applications. in SD Miller & RG Ross, Jr. (eds), Proceedings of the 14th International Cryocooler Conference (ICC 14) 14-16 June 2006, Annapolis, Maryland, USA. ICC Press, Boulder CO, pp. 75-82, 14th International Cryocooler Conference (Cryocoolers 14), June 14-16, 2006, Annapolis, MD, USA, Annapolis, MD, United States, 14/06/06.

Design of a large heat lift 40 K to 80 K pulse tube cryocooler for space applications. / Trollier, T.; Tanchon, J.; Buquet, J. et al.
Proceedings of the 14th International Cryocooler Conference (ICC 14) 14-16 June 2006, Annapolis, Maryland, USA. ed. / S.D. Miller; R.G. Ross, Jr. Boulder CO: ICC Press, 2007. p. 75-82.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

TY - GEN

T1 - Design of a large heat lift 40 K to 80 K pulse tube cryocooler for space applications

AU - Trollier, T.

AU - Tanchon, J.

AU - Buquet, J.

AU - Ravex, A.

AU - Charles, I.

AU - Coynel, A.

AU - Duband, L.

AU - Ercolani, E.

AU - Guillemet, L.

AU - Mullié, J.

AU - Dam, J.A.M.

AU - Benschop, T.

AU - Linder, M.

PY - 2007

Y1 - 2007

N2 - A Large heat lift Pulse Tube Cooler (LPTC) is under development in partnership with AL/ DTA, CEA/SBT and THALES Cryogenics. The engineering model is expected to provide 2.3 W at 50 K at a 10 °C rejection temperature and 160 watts of electrical input power to the compressor. The split coaxial design of the pulse tube cold finger and the moving magnet linear motor compressor design will be presented. The expected thermal and mechanical performances will be also discussed. The engineering model will be delivered to ESA/ESTEC in October 2006 after completion of a qualification test program. This work is funded by the European Space Agency (ESA/ESTEC Contract N° 8433/04/NL/AR) for future earth observation instrument missions.

AB - A Large heat lift Pulse Tube Cooler (LPTC) is under development in partnership with AL/ DTA, CEA/SBT and THALES Cryogenics. The engineering model is expected to provide 2.3 W at 50 K at a 10 °C rejection temperature and 160 watts of electrical input power to the compressor. The split coaxial design of the pulse tube cold finger and the moving magnet linear motor compressor design will be presented. The expected thermal and mechanical performances will be also discussed. The engineering model will be delivered to ESA/ESTEC in October 2006 after completion of a qualification test program. This work is funded by the European Space Agency (ESA/ESTEC Contract N° 8433/04/NL/AR) for future earth observation instrument missions.

M3 - Conference contribution

SN - 978-1-934021-00-2

SP - 75

EP - 82

BT - Proceedings of the 14th International Cryocooler Conference (ICC 14) 14-16 June 2006, Annapolis, Maryland, USA

A2 - Miller, S.D.

A2 - Ross, Jr., R.G.

PB - ICC Press

CY - Boulder CO

T2 - 14th International Cryocooler Conference (Cryocoolers 14), June 14-16, 2006, Annapolis, MD, USA

Y2 - 14 June 2006 through 16 June 2006

ER -

Design of a large heat lift 40 K to 80 K pulse tube cryocooler for space applications

Abstract

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