Archive for the “Blackbodies” Category

Ircon, Inc., a leading producer of industrial radiation thermometers, line scanners and quantitative thermal imagers, in its training programs for many years used to teach something they called the RAT Theory.

Reflectance, Absorbtance and Transmittance, or the coefficients of them, abbreviated as R, A &T must sum to 100%, or R + A + T=1.

An easy way for newcomers to Infrared radiation thermometry to remember a very important concept.

The associated concept is that Absorbtance=Emittance, or A=E. Or the RAT theory could be written as R+E+T=1 and renamed the RET Theory.

So, while not as easily recalled, the RET Theory name just didn’t catch on as easily as the RAT Theory.

(BTW, whenever I tried to teach some basics of Radiation Thermometry, I used to call it the TAR Theory because I thought it might “stick” better- it didn’t - RAT wins by a landslide every time.)

Al this is a lead in to the wonderful resources by the folks at  LabSphere for those who want to know or learn how to measure emittance or absorbtance through the roundabout way of measuring reflectance and transmittance first and then doing a bit of math.

They have a readily downloadable 26 page PDF document entitled “A Guide to Integrating Sphere Radiometry and Photometry”.

It explains far more than the RAT or RET or TAR theories about optical radiation metrology.

I think it and many of their online aids are well worth a read.

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A Search on the NASA website results in the following abstracts

 

DETERMINATION OF THE EMISSIVITY OF MATERIALS

Author(s): Askwyth, W. H.
Abstract: Space power systems - emissivity of candidate materials for snap-8 powerplant
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2006-11-06
Accession Number: 63N11697; Document ID: 19630001823; Report Number: PWA-2088

Determination of emissivity of materials quarterly progress report, 1 jul. - 30 sep. 1962

Author(s): Askwyth, W. H.; Hayes, R. J.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2006-11-06
Accession Number: 67N83465; Document ID: 19670084086; Report Number: NASA-CR-83756, PWA-2128

EMITTANCE OF MATERIALS SUITABLE FOR USE AS SPACECRAFT RADIATOR COATINGS

Author(s): Askwyth, W. H.; Hayes, R. J.; Mikk, G.
Abstract: Emittance measurements of materials suitable for spacecraft radiator coatings
NASA Center: NASA (non Center Specific)
Publication Year: 1963
Added to NTRS: 2006-11-06
Accession Number: 63A24987; Document ID: 19630028928

Measurement of spectral normal emittance of materials under simulated spacecraft powerplant operating conditions

Author(s): Askwyth, W. H.; House, R. D.; Lyons, G. J.
Abstract: Spectral normal emittance of materials under simulated space environment
NASA Center: NASA (non Center Specific)
Publication Year: 1963
Added to NTRS: 2006-11-06
Accession Number: 64N10959; Document ID: 19640001050

THE EMITTANCE OF MATERIALS SUITABLE FOR USE AS SPACECRAFT RADIATOR COATINGS

Author(s): Askwyth, W. H.; Hayes, R. J.; Mikk, G.
Abstract: Emittance of materials suitable for use as spacecraft radiator coatings
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2006-11-06
Accession Number: 63N10264; Document ID: 19630000390; Report Number: ARS PAPER-2538-62

THE EMITTANCE OF MATERIALS SUITABLE FOR USE AS SPACECRAFT RADIATOR COATINGS

Author(s): Askwyth, W. H.; Hayes, R. J.; Mikk, G.
Abstract: Measurements of total hemispherical emittance for materials suitable for high-temperature spacecraft radiation coatings
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2006-11-06
Accession Number: 63A11692; Document ID: 19630015633; Report Number: ARS PAPER 62-2538

A SIMPLE TECHNIQUE FOR DETERMINING TOTAL HEMISPHERICAL EMITTANCE BY COMPARING TEMPERATURE DROPS ALONG COATED FINS

Author(s): Askwyth, W. H.; Curry, R.; Lundberg, W. R.
Abstract: Determination of total hemispherical emittance by comparing temperature drops along coated fins
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2006-11-06
Accession Number: 62N17085; Document ID: 19620007085

Measurement of total hemispherical emittance of structural materials and coatings under simulated spacecraft conditions

Author(s): Askwyth, W. H.; Mikk, G.
Abstract: Hemispherical emittance of structural materials and amp coatings under simulated spacecraft conditions over wide temperature range
NASA Center: NASA (non Center Specific)
Publication Year: 1963
Added to NTRS: 2006-11-06
Accession Number: 64N10962; Document ID: 19640001053

Determination of the emissivity of materials

Author(s): Askwyth, W. H.; Hayes, R. J.; House, R. D.; Mikk, G.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1962
Added to NTRS: 2004-11-03
Accession Number: 76N78693; Document ID: 19760073652; Report Number: NASA-CR-148751, PWA-2206(VOL.1)

Determination of the emissivity of materials

Author(s): Askwyth, W. H.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1961
Added to NTRS: 2004-11-03
Accession Number: 82N70372; Document ID: 19820065104; Report Number: NASA-CR-164941, PWA-2043

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Introductory Guide to Emissivity

Sketch of the concept of spectral emissivity measurement
This is an introductory page on the National Physical Laboratory (NPL) website in the UK.

It has several such sketches as on the left showing the concept of the “radiometric method” of emissivity measurement and discusses both the concepts and measurement methods used to quantify spectral and total emissivity values.

The page also features links to other resource materials on the subject and a list of reference books.

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It is not an oxymoron, nor a quote from Yogi Berra.

Real Blackbodies do not exist, at least on Earth. Only approximations or simulations are real. We use them to calibrate IR Thermometers, Radiation Pyrometers and Thermal Imagers.

Technically they should have a spectral emissivity very close to 1.0. How close, you might ask? Read on.
Max Planck needed the concept of a perfect absorber of electromagnetic, thermal radiation to develop his theory of Thermal Emission of Radiation in 1899. Fortunately, Gustav Kirchhoff had already develped the foundation for them forty years earlier.

A perfect blackbody is perfectly absorbing to all the thermal radiation incident upon it. For that reason it had, necessarily, to be opaque and non-reflecting.

By logical reasoning, it was also clear that the same device had to be a perfect emitter of thermal radiation related to its absolute temperature, that is, temperature on the Absolute or Kelvin Temperature Scale.

There are several radiation equations or “Laws” that have been developed to describe the physics of thermal emission properties. They are well explained in a number of texts and shown in some detail in the online Hyper Physics website.

In an online Java applet, one can see visually also the three main radiation laws in graphic action; the temperature on the screen is shown on a column in a thermometer on the right side, and you can change it by clicking and/or dragging on it with your mouse.

If someone asks about the color of a blackbody, you can always refer them to this great set of webpages by Mitchell Charity at MIT.
They show both the temperature from 1000 K to 29,800 K (of course below about 700 K blackbodies actually look black to the human eye) . As can be seen on this page, red, white and blue blackbodies are possible!

There aren’t many 29,800 K blackbodies on Earth, but astronomers & AstroPhysicists see them all the time. How do you think they measure the temperatures of stars?

So, now you know, there can be both Red and Blue Blackbodies!

The devices used by calibration laboratories to calibrate and check the calibration of IR Thermometers, Radiation Thermometers and Infrared Thermal Imagers are not perfect (and seldom Blue, but often appearing Black, Red, Orange, Yellow and even White), but they can be very close to perfect.

The closer to perfection, the higher the cost of them also.

A blackbody having a spectral emissivity of 0.99 would have, at best, an error of about ± 1% in emitted thermal radiation or radiance, at a stable operating temperature and could be used to calibrate Infrared Thermometers.

The thermometers would be limited in their calibration uncertainty, since the radiance they emit would be uncertain to at least ± 1%.

Depending upon the radiance to temperature relationship for the temperature in question, that could mean a bigger or smaller effective temperature calibration uncertainty that could be assigned to a thermometer being calibrated.

That’s another issue for another time, but , if you can’t wait, one of the best explanations (and a lot more) that we have seen on that subject is in a 547 KB, downloadable PDF file from Land Instruments.

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