Many present and future NASA missions require high-performance, large-scale cryogenic systems, such as the sunshields and cold instruments for the James Webb Space Telescope (JWST). Testing these systems is problematic because of both the size and the low heat loads allowed. The heat loads can be greatly influenced by non-ideal blackbody characteristics of the test chamber, and by stray heat from warmer parts of the system and ground support equipment. Previously, stray thermal energy was not directly measured, but inferred from deviations in the expected results, which leads to errors in thermal modeling and in lack of knowledge of the thermal performance of the item under test. Technologists at NASA Goddard Space Flight Center have developed a radiometer to help identify the sources of stray heat and to make non-contact thermal emission measurements of such materials as vapor-deposited aluminum on Kapton and multilayer insulation blankets, as well as background measurements of non-ideal chamber effects such as light leaks and radiation bounces.

Cut-away drawing of the radiometer, electrical connector, and bracket. The length of the radiometer in this version is about 50 mm. Note the two thermometers (black) in the lower portion. For ease of drawing, the upper portion of the Winston cone is shown as cylindrical rather than parabolic.

The radiometer is a simpler, much cheaper, and more flexible version of infrared detectors that have been in use for very-high-resolution astronomical observations. Its form is similar to bolometers, which have long been used for sensitive astronomical infrared measurements. By relaxing the sensitivity and response times, the radiometers can be made much less costly.

The device is composed of a non-imaging concentrator, known as a Winston cone, and a pair of thermometers that all reside at low temperature. The radiometer was designed to help identify the sources of stray heat and to make non-contacting thermal emission measurements of various materials. The Winston cone is made from ordinary Aliminum alloy (e.g. 6061-T6) with an entrance aperture of about 17 mm wide and an exit aperture of about 3 mm in diameter. Light entering the Winston cone exits through this aperture into a cavity in which is suspended a small thermometer. This thermometer will be coated with a stainless-steel-powder-loaded epoxy to achieve relatively high emissivity. This coating has the property of nearly wavelength independent absorption over the wavelength range from a few microns to more than 100 microns. A second matching thermometer is located on the back and outside the cavity. Using the two thermometers together provides a calibratable readout that is insensitive to absolute temperature to first order.

The technology has several potential applications, including in situ sensing for long-wavelength infrared radiation, and looking for heat leaks and reflected flux in low-temperature thermal vacuum systems.

NASA is actively seeking licensees to commercialize this technology. Please contact the Strategic Partnerships Office at This email address is being protected from spambots. You need JavaScript enabled to view it. to initiate licensing discussions. Follow this link for more information: .

NASA Tech Briefs Magazine

This article first appeared in the July, 2016 issue of NASA Tech Briefs Magazine.

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