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Radiometer
Radiometer
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An example of a Crookes radiometer. The vanes rotate when exposed to light, with faster rotation for more intense light, providing a quantitative measurement of electromagnetic radiation intensity.

A radiometer is an instrument for measuring radiometric quantities such as radiant flux (power), irradiance, or radiance.[1] Definitions typically limit radiometry to optical radiation, but some definitions include other kinds of electromagnetic radiation. Radiometers typically measure infrared radiation, visible radiation (light), ultraviolet radiation, or some combination of these.[2][3][4]

Microwave radiometers operate in the microwave wavelengths. A roentgenometer is a radiometer for measuring the intensity of X-rays or gamma radiation.

While the term radiometer can refer to any device that measures electromagnetic radiation (e.g. light), the term is often used to refer specifically to a Crookes radiometer ("light-mill"), a device invented in 1873 in which a rotor (having vanes which are dark on one side, and light on the other) in a partial vacuum spins when exposed to light. A common misbelief (one originally held even by Crookes) is that the momentum of the absorbed light on the black faces makes the radiometer operate. If this were true, however, the radiometer would spin away from the non-black faces, since the photons bouncing off those faces impart more momentum than the photons absorbed on the black faces. Photons do exert radiation pressure on the faces, but those forces are dwarfed by other effects. The currently accepted explanation depends on having just the right degree of vacuum, and relates to the transfer of heat rather than the direct effect of photons.[5][6]

A Nichols radiometer demonstrates photon pressure. It is much more sensitive than the Crookes radiometer and it operates in a complete vacuum, whereas operation of the Crookes radiometer requires an imperfect vacuum.

The MEMS radiometer can operate on the principles of Nichols or Crookes and can operate over a wide spectrum of wavelength and particle energy levels.[7]

See also

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References

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from Grokipedia
A radiometer is an instrument for detecting and measuring the intensity of , such as or other . A well-known example is the , often simply called a radiometer, consisting of an airtight bulb containing a partial and a rotor with four vanes that rotate when exposed to or other . Each vane is typically diamond-shaped, with one side coated black to absorb and the opposite side reflective or white to reflect it, mounted on a low-friction pivot for free . Invented in 1873 by British chemist and physicist , the emerged as a byproduct of his quantitative chemical experiments on the element , where he noticed light unexpectedly affecting sensitive balance measurements. Crookes' work built on his earlier inventions, such as the for studying , and the radiometer quickly became a subject of fascination among 19th-century scientists, including James Clerk Maxwell and , who contributed to debates on its underlying mechanism. Initially misinterpreted as evidence of direct from photons, the device's motion puzzled researchers for decades until explanations involving effects were refined. The principle of operation relies on the radiometric force, or thermal transpiration, arising from the temperature difference between the vane surfaces in the low-pressure environment (typically around 1 Pa). The black surface absorbs , heating up more than the reflective side and warming adjacent gas molecules, which then rebound with greater and impart a on the vane, causing it to rotate with the black side trailing. This effect requires residual gas in the bulb—full halts rotation—and is most pronounced with infrared radiation, though also works via heating. Modern analyses, including those using the Einstein effect and thermal creep models, confirm this thermal origin over pure momentum. Beyond its historical role, the Crookes radiometer serves as an educational tool in physics to illustrate , gas kinetics, and radiation interactions, and has inspired applications in microscale and , such as light-driven rotors at . It remains a staple in science museums and laboratories, highlighting serendipitous discovery in scientific progress.

Overview

Definition

A radiometer is an instrument designed to detect and quantify , typically such as , , or microwaves. It measures the intensity of this , often expressed in units of watts per square meter (W/m²) for . Radiometers are passive devices that generate observable responses, such as mechanical motion or electrical signals, upon absorbing incident . They directly assess levels across defined bands. Radiometers are broadly classified into thermal types, which operate based on heating and changes in the detector , and quantum types, which respond to individual photons exciting charge carriers, such as through photodiodes that convert light directly into electrical current via the . Originating in 19th-century investigations into phenomena, radiometers evolved from qualitative devices, exemplified by the Crookes radiometer's mechanical in response to light, to sophisticated tools for precise measurements in fields like astronomy and .

Basic Components

Radiometers, as instruments for measuring , typically incorporate a to contain and direct the , absorbing surfaces to capture incident , and a support structure to position these elements stably. The often consists of a sealed enclosure, such as a glass in radiometers or an in optical standards, which may be evacuated to a partial of approximately 1 Pa in designs requiring minimal gas interference, like those with rotating vanes. Absorbing surfaces form the core detection elements, featuring high-absorptivity coatings—such as blackened or soot-covered areas—to efficiently capture . In non-mechanical variants, these surfaces integrate specialized detectors, including thermopiles for solar measurements or bolometers for sensitive detection, often paired with wavelength-selective filters to isolate specific bands. Support structures, such as low-friction pivots or spindles in rotating types, or fixed mounts in stationary setups, ensure precise alignment and minimal mechanical interference. Electronic radiometers commonly include amplifiers and signal readouts to process detector outputs, enhancing sensitivity for low-flux environments, while microwave variants feature antennas or apertures as primary collectors alongside low-noise amplifiers. Calibration of these components relies on blackbody sources to establish absolute accuracy, with standards achieving uncertainties as low as 0.3% in spectral responsivity for optical systems.

History

Early Concepts and Precursors

Early observations of solar heating date back to philosophers, who qualitatively described the warming effects of without quantitative measurement or understanding of underlying mechanisms. For instance, remarked on the sun's ability to heat homes oriented southward during winter, highlighting an early recognition of directional thermal influences from celestial sources. These ideas, echoed in the elemental theories of figures like —who posited fire as a fundamental root associated with solar phenomena—laid conceptual groundwork for later scientific explorations of , though they remained philosophical rather than instrumental. In the late 18th and early 19th centuries, precursors to radiometers emerged as devices for visualizing and detecting , driven by advances in . John Leslie introduced the in 1804, a hollow metal container filled with hot water to demonstrate differences in emission from surfaces of varying finishes, such as matte black, polished metal, and painted sides, using a sensitive to compare intensities. This apparatus provided a controlled blackbody-like source for studying radiative properties, marking a shift toward empirical investigation of propagation without contact. Building on this, Macedonio Melloni developed the thermomultiplier in the 1830s, an early comprising multiple bismuth-copper thermocouples connected in series to amplify weak thermal signals, capable of sensing from a at distances up to 30 feet. The scientific context for these precursors was shaped by foundational discoveries in and the demands of the , which necessitated precise tools for managing in engines and machinery. The Seebeck effect, discovered by in 1821, revealed that a difference between junctions of dissimilar metals generates an , enabling the creation of thermopiles as sensitive detectors for radiant . Concurrently, early studies of , initiated by Pierre Prévost's 1791 theory of exchanges between hot and cold bodies, emphasized the universal nature of thermal emission, influencing experiments on during an era of rapid industrialization. These developments addressed the growing need for quantitative measurement amid steam engine innovations and manufacturing expansions. Despite their innovations, these early devices served primarily as sensors for detection and visualization, lacking integrated mechanical motion to demonstrate radiometric forces, which limited their ability to provide dynamic insights into interactions. Such constraints highlighted the demand for more holistic instruments that could exhibit tangible responses to incident , paving the way for later integrated designs.

Invention and Key Developments

Sir William Crookes, a British and , invented the first practical radiometer in 1873 while using a sensitive balance to determine the atomic weight of , where he observed unexpected rotational motion in the device when exposed to or , which initially puzzled him and led him to hypothesize an effect from . He detailed this discovery in a seminal paper presented to the Royal Society in 1873 and published in 1874, marking the radiometer's transition from a chemical research byproduct to a recognized . Crookes secured a U.S. for an improved version of the apparatus in 1876, emphasizing its utility in indicating intensity. The anomalous motion of sparked intense debate among physicists, with early explanations attributing it to light pressure, as proposed by James Clerk Maxwell. In 1874, British engineer Osborne Reynolds provided a more accurate theoretical framework in a paper to the Royal Society, introducing the concept of thermal transpiration—whereby gas molecules in a partial flow from colder to hotter regions due to temperature gradients, driving the vanes' rotation. In 1910, provided further insight through a kinetic analysis, explaining the radiometer's behavior in terms of molecular momentum transfer from the heated surfaces to adjacent gas molecules. This explanation resolved the mystery and laid the groundwork for understanding thermal effects in low-pressure environments, influencing subsequent radiometer designs. A significant advancement came in 1901 with the Nichols radiometer, developed by American physicists Ernest Fox Nichols and Gordon Ferrie Hull to precisely measure from light sources. Unlike Crookes' device, which relied on mechanical motion in a partial , the Nichols instrument used delicately suspended absorbing and reflecting vanes in a high to detect from momentum, achieving sensitivities sufficient to confirm Maxwell's predictions quantitatively. This innovation shifted radiometers toward more accurate optical and photometric applications, bridging demonstration tools and precision measurement instruments. In the 1930s and 1940s, the advent of technology enabled the development of electronic radiometers, which amplified weak signals from radiation detectors for improved sensitivity and quantitative analysis. These devices, building on principles, replaced purely mechanical systems with electronic amplification, facilitating broader use in and early radio detection. During , microwave radiometer technology advanced rapidly at facilities like MIT's Radiation Laboratory, where researchers refined sensitive receivers for systems to measure atmospheric microwave absorption and noise, enhancing wartime detection capabilities. Postwar innovations culminated in space-age adaptations, such as the Infrared Interferometer Spectrometer and Radiometer (IRIS) instrument on NASA's Voyager probes, launched in 1977. This radiometer measured thermal emissions and cosmic radiation spectra from planetary atmospheres and interstellar space, providing unprecedented data on solar system bodies and the during Voyager's grand tour. These developments transformed the radiometer from a Victorian into a cornerstone of modern and .

Operating Principles

Thermal Effects in Radiometers

In the Crookes radiometer, incident radiation, particularly visible and infrared light, is absorbed primarily by the black-coated surfaces of the vanes, leading to a localized temperature increase. The black coating enhances absorptivity, converting radiant energy into heat more efficiently than the reflective opposite side. This differential absorption creates a temperature gradient across each vane, with the black side heating to higher temperatures (typically a few degrees Celsius above ambient under moderate illumination). The temperature difference arises because the black surface absorbs while the reflective side bounces it away, minimizing heating. In the partial inside the (around 0.01 or 10 Pa), heat dissipation from the vanes occurs mainly through conduction to the pivot and to the enclosure, with limited due to low gas . This environment sustains the thermal gradient, as the residual gas molecules interact with the heated surfaces without rapid equalization via bulk flow. The gradient is crucial for the subsequent radiometric force, as it influences the behavior of gas molecules near the vane edges and surfaces. At under continuous illumination, the difference stabilizes when input balances losses, resulting in a consistent ΔT proportional to the incident intensity. Full would eliminate gas-mediated effects, halting , while higher pressures increase convective cooling, reducing the and altering motion direction.

Radiometric Force and Motion

The radiometric force originates from the uneven transfer by gas molecules to a surface subjected to a in a partial . Molecules incident from the ambient gas impart greater to the hotter side of the surface due to thermal accommodation, where they absorb and re-emit with higher average velocity, resulting in a net force directed from the cold side toward the hot side. This phenomenon is prominent when the molecular is comparable to the surface dimensions, typically in rarefied gases. In a simplified model derived from kinetic theory for the free-molecular , the radiometric FF on a surface is approximated as FP2ΔTTA,F \approx \frac{P}{2} \frac{\Delta T}{T} A, where PP is the gas , ΔT\Delta T is the temperature difference between the hot and cold sides, TT is the ambient temperature, and AA is the effective surface area. This expression captures the linear dependence on and the relative , assuming full thermal accommodation and small ΔT/T\Delta T / T. More detailed formulations, such as those incorporating , adjust for transitional flow regimes but retain this core scaling. In the , the radiometric force induces rotational motion of the vanes, where the blackened sides absorb light and become hotter, leading to elevated on the hot side that pushes against the cooler side, generating . The assembly rotates such that the hot (blackened) sides trail, with typical speeds reaching hundreds of RPM under illumination in optimal partial conditions. The direction of rotation reverses in full , where residual dominates but is negligible, or at high pressures, where collisional effects and alter the force balance. Early theoretical explanations evolved from ' initial attribution to direct , which was refined by James Clerk Maxwell in 1879 through his analysis of thermal stresses in rarefied gases, introducing the concept of thermal slip at boundaries. Osborne Reynolds further clarified the mechanism in 1879 by proposing thermal creep (or thermal transpiration), where gas flows along the from cold to hot over surface edges or pores due to differences in molecular effusion rates. Modern understanding, grounded in kinetic theory, integrates these via the , resolving the force as a combination of normal (Einstein effect) and tangential creep, with numerical solutions confirming the edge-dominated contributions in transitional Knudsen numbers (0.1–10). The radiometric force exhibits significant limitations tied to pressure-dependent mean free path lengths. It diminishes at very low pressures (< 10310^{-3} Pa), approaching ballistic molecular motion where insufficient collisions prevent sustained gradients. At high pressures (>100 Pa), frequent intermolecular collisions enforce continuum flow, suppressing the nonequilibrium effects essential for the force. Peak performance occurs around 1 Pa, where the balances area and edge contributions optimally.

Types

Crookes Radiometer

The consists of four thin vanes, typically 3–5 cm in diameter, with one side blackened for light absorption and the other silvered for reflection, arranged horizontally and mounted on a low-friction pivot or spindle inside a sealed glass bulb evacuated to a partial of approximately 1 Pa. This design allows the vanes to rotate freely when exposed to , converting into mechanical motion through interaction with the residual gas molecules. Under illumination, the vanes rotate such that the blackened sides trail, achieving speeds up to 1000 RPM in direct sunlight, with the rotation rate increasing proportionally to light intensity. The device exhibits peak sensitivity to wavelengths in the visible and near-infrared ranges, where absorption by the blackened surfaces generates the necessary temperature gradient for motion. Modern construction variations include replicas with bulbs to enable transmission of light, enhancing responsiveness to shorter wavelengths. Quantitative versions incorporate mechanisms to measure speed, allowing calibration against levels for more precise light intensity assessments. A persistent misconception attributes the radiometer's to direct momentum transfer from photons, akin to ; however, this is orders of magnitude too weak to produce the observed effect. Instead, the motion stems from effects involving gas interactions at the vane edges, as confirmed by experiments showing optimal at low pressures around 1 Pa, cessation in high due to insufficient gas, and reversal or halting at .

Pyranometers and Solar Radiometers

Pyranometers are specialized radiometers designed for precise measurement of global on a horizontal surface, typically within the spectral range of 0.3 to 3 μm. They feature a housed within a double glass dome enclosure, which protects the detector while allowing a 180° hemispherical to capture both direct and diffuse . The outer dome reduces convective losses, while the inner dome minimizes thermal offsets from environmental variations. The consists of multiple junctions that generate a voltage proportional to the difference induced by absorbed . In operation, the hot junctions of the are positioned beneath a black absorber coating that captures nearly all incident shortwave , converting it to and raising the of these junctions. The cold junctions are thermally coupled to the instrument body or, in black-and-white designs, to a white reflector surface that minimizes absorption of ambient , thereby reducing zero-offset errors. The domes facilitate a cosine response, ensuring the sensor's output accurately represents regardless of the sun's angle of incidence, as the diffuse light to approximate the ideal cosine law for . The II (in W/m²) is calculated from the output voltage VV (in V) and the instrument's calibrated sensitivity SS (in V/(W/m²)) using the equation I=V/SI = V / S. Solar-specific variants extend functionality for net radiation balance assessments. Net radiometers incorporate upward- and downward-facing sensors to separately measure incoming () and outgoing () shortwave and fluxes, enabling calculation of budgets. Albedometers, typically comprising paired —one facing upward to detect global irradiance and the other downward to capture reflected —quantify surface as the ratio of to solar . Calibration of pyranometers is performed against reference pyrheliometers under clear-sky conditions at approximately 500 W/m² , ensuring traceability to the World Radiometric Reference. According to ISO 9060:2018, Class A instruments achieve an overall accuracy of ±2% for , directional, and response, making them suitable for high-precision solar monitoring.

Microwave Radiometers

Microwave radiometers operate in the range of 1 to 100 GHz, employing superheterodyne receivers paired with square-law detectors to measure weak thermal emissions. A key component is the Dicke switch, which alternates between the antenna signal and a stable load to mitigate gain fluctuations and receiver , enabling precise calibration of the . This configuration, often implemented in balanced or unbalanced forms, ensures high stability by continuously comparing the incoming signal against the , effectively canceling out common-mode sources. In operation, these radiometers quantify the intensity of microwave radiation through the concept of brightness temperature TBT_B, leveraging the Rayleigh-Jeans approximation valid at microwave frequencies where the Planck function simplifies to a linear relation with temperature. The spectral radiance IνI_\nu is thus given by: Iν=2kTBν2c2I_\nu = \frac{2 k T_B \nu^2}{c^2} where kk is Boltzmann's constant, ν\nu is the frequency, and cc is the speed of light. This approximation allows the radiometer to infer TBT_B directly from the detected power, providing a measure of the scene's effective temperature without needing absolute intensity calibration. Specialized variants include polarimetric microwave radiometers, which utilize orthogonal feeds to capture vertical and horizontal polarizations, enabling the derivation of for analyzing polarization states in emitted radiation. Additionally, correlation radiometers extend this capability for interferometric applications by computing the between signals from separate antennas, facilitating high-resolution imaging through techniques. The sensitivity of microwave radiometers is characterized by the noise equivalent temperature difference ΔT\Delta T, which determines the smallest detectable change in . This is approximated as: ΔTTsysBτ\Delta T \approx \frac{T_{sys}}{\sqrt{B \tau}}
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