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Interior/Exterior Artist rendering of Columbus Laboratory Module for the International Space Station

 

Refrigerator/Freezer Rack (RFR) Highlighted areas depict placement of Marlow Industries designed finned heat exchanger units

 

Image of finned heat exchanger unit for RFR

 

Marlow Develops Refrigerator Freezer Racks for the International Space Station

  The International Space Station serves mainly as a research laboratory that can provide the special conditions of space on a permanent basis. The space station program will aim at a successful multidisciplinary utilization of the space station in the fields of research in space, technology, geoscience and space exploration. In order to accomplish this daunting mission, the station will be equipped with Columbus, a space laboratory scheduled for last module placement sometime in 2004. Nearly 8 meters in length and 4.5 meters in diameter, the module will house 10 International Standard Payload Racks (ISPRs) designed for a variety of applications including communications, power supply and temperature control. Once deployed this module will be instrumental in space based research for an estimated operational lifespan of over 10 years.

Marlow Industries has lent its extensive experience in space-based thermoelectrics to the development of the Refrigeration Freezing Rack (RFR). The RFR is a specially designed refrigerator/freezer that will be used by astronauts on the Space Station for food storage and transportation. Marlow has custom designed finned heat exchangers to cool the RFR. To avoid frost on the fins, a system has been included to eliminate water by capillarity.

General Information on Space Refrigeration/Freezing

  Refrigerator/freezer applications for space applications are usually found in three varieties. These are deep freezing of food or samples (-30°C), refrigeration to 4°C, and incubators (40°C to 4°C). Marlow provides a heat exchanger (air-to-air or water-to-air) using thermoelectric coolers as the active cooling or heating component. This application requires a close working relationship with our customer because of the need to coordinate the fans and the interface with the heat exchanger. These applications require high-performance products and are produced in low volume (fewer than 10 units). They are custom products and are not cost-sensitive.

Advantages of Thermoelectrics for this Application

  The advantage of thermoelectrics is the use of solid-state technology that does not require Freon or bearings that contain oil. Due to the restrictions on Freon and oils in the space equipment, compressor-based systems are expensive and unreliable. Thermoelectrics, while less efficient from a electrical/thermal standpoint, offer dramatically improved reliability and safety. In addition, thermoelectric coolers have an excellent track record in space applications. In the case of incubators, thermoelectric coolers are ideal as they can provide both heating and cooling.

Specific Marlow Advantages

  Space systems must be power-efficient for a given set of design parameters. To improve electrical efficiency, there must be considerable optimization to the thermoelectric cooler, heat sinks, fans, and interfaces. This requires extensive modeling experience and capability. Marlow has this experience, along with test and assembly experience. Marlow also has high-performing TE material that improves the electrical thermal performance of the assembly. Improvements in coefficient of performance of 10% to 20% over our competitors' TE coolers are common.

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