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AMS02 Tracker Thermal Control System (TTCS) Design, Model and Breadboard Results
Technical Paper
2004-01-2556
ISSN: 0148-7191, e-ISSN: 2688-3627
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English
Abstract
The AMS Tracker Thermal Control System (TTCS) is a two-phase cooling system developed by NIKHEF (The Netherlands), Geneva University (Suisse), INFN Perugia (Italy), Sun Yat Sen University Guangzhou (China) and NLR (The Netherlands). The TTCS is a mechanically pumped two-phase carbon dioxide cooling loop. Main objective is to provide accurate temperature control of AMS Tracker front-end electronics. Additional objective is to prove and qualify a two-phase pumped cooling in orbit and collect operational data in μ-g environment over a period of three years. The paper describes the concept selection, breadboard results and an outlook to the experiments in orbit.
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Authors
- J. van Es - National Aerospace Laboratory NLR, The Netherlands
- G. van Donk - National Aerospace Laboratory NLR, The Netherlands
- A. Pauw - National Aerospace Laboratory NLR, The Netherlands
- C.A.M. Rens - National Aerospace Laboratory NLR, The Netherlands
- J. Jaarsma - National Aerospace Laboratory NLR, The Netherlands
- M.P.A.M. Brouwer - National Aerospace Laboratory NLR, The Netherlands
- B. Verlaat - National Institute for Nuclear and High Energy Physics, NIKHEF
Citation
van Es, J., van Donk, G., Pauw, A., Rens, C. et al., "AMS02 Tracker Thermal Control System (TTCS) Design, Model and Breadboard Results," SAE Technical Paper 2004-01-2556, 2004, https://doi.org/10.4271/2004-01-2556.Also In
References
- Delil, A.A.M. Research issues on Two-Phase Loops for Space Applications Proc. ISAS Symp. On Space Flight Mechanics Sagamihara, Japan 2000
- Verlaat B. Rookhuizen H. Boer Delil A.A.M. Woering A.A. Perrin E. Pohl M. Feasibility Demonstration of a Mechanically Pumped Two-Phase CO2 Cooling Loop for the AMS-2 Tracker Experiment
- Delil, A.A.M. Pauw A. Woering A.A. Verlaat B. AMS-2 Tracker Thermal Control System: Design and Thermal Modellling of the Mechanically Pumped Two-Phase CO2 Loop, Proc. 2003 Albuquerque, NM, USA
- Akachi, H Polashek, F. ‘Pulsating heat pipes; a new challenge in heat pipe technology” 9th Int. Heat Pipe Conf. Albuquerque, New Mexico 1995
- Ochterbeck, J.M. “Reduced Gravity Testing of an Oscillatory (Pulsating) Heat Pipe International Two-Phase Thermal control Technology Workshop El Segundo 2001
- Miyasaka et al 1996
- Van Es, J. Woering A.A. “High-acceleration performance of the Flat Swinging Heat Pipe 30th Int. Conf. on Environmental Systems” Toulouse, France 2000
- Kandhekar, S. Groll M. On the definition of Pulsating Heat Pipes: An Overview Proc. 5 th Minsk Int. Seminar (Heat Pipes, Heat Pumps and Refrigerators) Minsk Belarus 2003
- Charoensawan et al. Effects of Inclination angles, Filling ratios and Total lengths Heat Transfer Characteristics of a Closed-loop Oscillating Heat Pipe 6th Int. Heat Pipe Symposium Chiang Mai, Thailand 2000 422 429
- Groll, M. Khandekar, Pulsating Heat Pipes: A challenge and still unresolved problem in heat pipe science Heat 2002 Baranow Sandomierski, Poland 2002