1 Introduction

Ultraviolet (UV) astronomy was born in the late sixties with the advent of space astronomy. Ever since, a well defined set of photometric standards has been carried over from mission to mission ensuring the accuracy and consistency of the data.

This controlled approach is going to change during the next decade with the advent of widespread use of cubesat technology. Access to UV data is fundamental in many areas of astrophysical research, however no pure UV observatories are included in the strategic planning of the main space agencies with the only exception of the Spektr-UF (WSO-UV, [39]) observatory from the Russian space science program, and the more distant NASA Habitable Worlds Observatory projected to fly in the 2040s. ULTRASAT [6] will be launched around 2025, and a MIDEX-class mission, UVEX, has been funded for a phase-A study [31]. Several other missions are under study, such as CASTOR [15] MESSIER [49], UV-SCOPE [2], HYPERION [26], and ASPERA [14], among others. CubeSats such as CUTE [21] have also been launched and it is expected. that many SmallSat- and CubeSat-scale missions will be flown to run well-defined experiments, including survey-type probes [see [23], for a recent compilation of the operational UV missions, those under construction and their main goals].

In this context, it is necessary to define some common foundations to facilitate comparing and contrasting data from different UV missions. From 2018 till 2021, the charter of the UV astronomy working group (UVA WG) of the International Astronomical Union (IAU) was to set the foundations for the definition of such standards: a UV photometric system suitable to be implemented from large to small missions and that grows with the scientific challenges addressed by using UV astronomical instrumentation.

Fig. 1
figure 1

Sketch outlining the spectral coverage of the UV filters (or bands) used for imaging purposes in astronomy (GALEX, Astrosat/UVIT, HST/ACS, HST/STIS, XMM-Newton/OM, SWIFT/UVOT). Note that the actual effective passbands also depend on the response of the detector. This is particularly relevant for the MCP type detectors, often used in UV Astronomy, since they use photocathodes only sensitive to specific spectral ranges. We refer the reader to the Instrument manuals and handbooks for more details on the filters (precise transmittance curves, effective wavelengths, etc.) in each case. Note that, for instance, several ACS filters are step filters that cannot be adequately represented in this plot. Also, the HST instruments possess many filters that have a high degree of spectral overlap

The recommendations made by the UVA WG were backed at the IAU General Assembly (Resolution B4Footnote 1) and approved with the strong support of the community. This article summarizes the contents of the report elaborated by the UVA WG during their study, as well as the description of the recommended photometric system itself. In Section 2, the contents of the astronomical databases in terms of photometric data at UV wavelengths are reviewed. The key technologies involved in shaping the UV bands are described in Section 3. The actual photometric system recommended by the IAU is described in Section 4 and the procedures for its implementation in Section 5. A short discussion on the main advantages and limitations of the system is included in Section 6. The procedures followed by the UVA WG to raise the opinion of the community are briefly summarized in Appendix for the historical record.

2 UV photometry from already-flown missions

The history of UV astronomy begins with small instruments deployed on the early space probes such as the Carruther’s lunar telescope [13]. The first purpose-built astronomical observatory was launched in 1972 by NASA: the Copernicus (OAO-3, [38]) mission. Copernicus was equipped with instrumentation for spectroscopy in the 90-315 nm spectral range. Subsequent missions have included the International Ultraviolet Explorer (IUE, [7]), 1978-1996, for UV spectroscopy in the 115-315 nm range, the Far UV Spectroscopic Explorer (FUSE, [36]), 1999-2007, for spectroscopy in the 90.5-119.5 nm range, the GALaxy Evolution eXplorer (GALEX, [35]), 2003-2012, for imaging and slit-less spectroscopy in the 135-280 nm range and the Hubble Space Telescope (HST) (https://www.stsci.edu/hst/), launched in 1990 and still operational, to observe in the 115-350 nm range both in imaging and spectroscopic modes. Also flown have been SWIFT/UVOT [22], XMM-Newton/OM [30] and Astrosat/UVIT [44] which had moderate UV photometric capabilities. In Fig. 1, the UV photometric bands (or filters) used by these missions for imaging purposes are outlined. Table 1 provides a summary, extracted from the metadata of the missions’ archives, of their sky coverage, number of field observed, and mean, median and total exposures for each filter. We programmatically queried the Milkuski Archive for Space Telescopes (MAST) Portal, requesting positions and exposure times for all observations taken in a given UV filter/instrument/mission combination, and then computed the median, average and total integration time. We also computed the total number of non-repeated fields within a healpix representation whose angular size was approximately one third of the FOV of each instrument, so that fields separated by less than a third of the FOV counted as a single field. Changes in the metadata account for the differences between the 2020 values presented in the original IAU report and the current Table 1.

Table 1 UV fields observed before May 2020

The properties of the filters are also summarized with \(\lambda _{c}\) (the pivot wavelength, as a measure of the central wavelength of a filter (see https://hst-docs.stsci.edu/wfc3ihb and [47]), is calculated considering the integrated system throughput), and their full-width at half maximum, \(\Delta \lambda \). The sky coverage and fields are displayed in Fig. 2 for some representative surveys, as extracted from an analysis of the metadata of their archives.

Not surprisingly, GALEX, the UV photometric surveyor, has provided the bulk of the information on the UV sky however, as shown in Fig. 2, the vast majority of the data concerning sources located within \(\pm 10^{\circ }\) of the galactic plane has been obtained by the spectroscopic missions and by SWIFT.

Another relevant issue is that there are no photometric measurements below 115nm. This lower wavelength limit is set by the reflective cut-off of the MgF\(_{2}\) material used for protective mirror coatings as well as for the sealing / protective window of the MCP detectors operating at wavelengths below 170 nm. There are MCP devices that operate “open faced” and do not suffer this limit, and extend down to 100nm or lower, but whose response is generally curtailed above 200nm (they are solar blind).

UV photometry is based on the fluxes measured by the TD1 satellite [46]; magnitudes and standard errors were derived from absolute fluxes by means of the calibration by [27]. Fluxes were measured in four bands with an effective width of \(\sim 33\) nm and centred at 156.5 nm, 196.5 nm, 236.5 nm, and 274.0 nm; however none reaches below 140 nm. As shown in Fig. 1, these bands have not been used much in later missions and, in practice, the spectrophotometric standards in the HST system are now the baseline for flux calibration at UV wavelengths.

The original spectrophotometric standards were defined by the IUE. They were incorporated later into the HST [10]; the 23 original calibration stars and their finding charts can be found in [48]. The conversion of the IUE spectra on the white dwarf primary spectrophotometric scale [11] is described by [8, 9].

Fig. 2
figure 2

Sky coverage of the observations made with Astrosat/UVIT/FUV_F148W, SWIFT/UVOT/UVW2, GALEX/FUV and GALEX/NUV. The total number of exposures in a given region is indicated by the color code

Fig. 3
figure 3

Distribution of UV photometric standards in the sky

The spectrophotometric standards can be accessed through CALSPECFootnote 2; only 46 of them have been observed in the full 115-400 nm spectral range and just 3 (including Vega) have been observed with FUSE (i.e. below 115 nm). Most of the sources are either A-type stars or white dwarf stars. Their main characteristics and spatial distribution on the sky are represented in Fig. 3.

In summary, there is no standard system concerning UV photometry. The most frequently available bands are the FUV band (about 140-180 nm) and the NUV band (about 190-250 nm), plus the u-band from the Strömgren photometric system (which is used to bridge the gap to the optical band). Very often, and especially at wavelengths below 200 nm, band selection is not implemented through the use of specific filters, since their construction has been very difficult to achieve. The absolute flux and cross talk calibration between missions and instruments is based on the well defined set of spectrophotometric standards maintained by the Hubble Space Telescope.

3 Foreseen characteristics of a UV photometric system suitable for small, cubesat-like missions

In this section, the main technological, environmental and astronomical issues taken into account for the definition of the UV photometric system are summarized. They will affect the definition of new missions when combined with cost-efficiency related issues.

Fig. 4
figure 4

Summary of photocathode quantum efficiency (QE, %) for opaque and semitransparent UV photocathodes. Comparison for an opaque CsI on a MCP, an opaque GaN on a sapphire substrate, a cutoff tailored NUV semitransparent bialkali on a MgF\(_{2}\) window, a typical Photonis high QE UV semitransparent bialkali on a fused silica window, and a semitransparent UV bialkali on a sapphire window in a Photonis Planacon MCP detector (https://www.photonis.com/system/files/2020-01/Leaflet_Quantum_Efficiency_Photocades.pdf). The percentage of ejected photoelectrons per impinging photons is represented in the Y-axis. Semitransparent photocathodes have been used in astronomical applications with efficiencies below 20% in the past. This technology has evolved significantly in the last decade. Depositing the photosensitive substrate directly in the MCP micro-tubes and slight variations in the micro-tubes geometry have proven to increase the efficiency by at least a factor of \(\sim 2\)

3.1 Detector and coating technology set the main instrumentation-related constraints

There are two widespread detector technologies used in UV astronomy: micro-channel plates (MCPs) and doped charge coupled devices (CCDs), and one emergent technology: complementary metal oxide semiconductor (CMOS). MCPs are photon counting devices based on a photocathode coupled to a micro-channel plate (MCP) that amplifies the electronic signal generating a shower of typically \(\sim 10^{5} - 10^{6}\) secondary electrons per photoelectron. This electron shower may be read directly using typically wedge- or cross-strip anodes, or transformed into optical photons and then read with conventional optically-coupled CMOS or CCD detectors. MCPs provide fast photon counting (\(\le \)10 milliseconds) and a well-defined spectral coverage determined by the photocathode material (often CsI or CsTe) and very good out-of-band rejection. In spite of their limitations (small dynamical range and limited lifetime), they have been implemented in most of the UV missions/instruments: GALEX, XMM-Newton/OM, SWIFT/UVOT, HST/ACS, HST/COS, Astrosat/UVIT. Their quantum efficiency is being improved by the use of materials such as GaN or new bi-alkali materials, or by the direct deposition of the photosensitive substrate on the MCP front face (see Fig. 4).

Fig. 5
figure 5

Quantum yield of the CCD without antireflection coating (blue) and with a correction for the quantum yield effect (green) after [43]

CCDs have flatter efficiencies over the UV range (see Fig. 5) and do not have a limited lifetime however, they are more sensitive in the visible than in the UV range. This becomes a problem, the so-called red-leak, when CCDs are used for UV photometric observation of bright optical sources. CCDs for UV astronomy require low working temperatures (140-170K) and are being used in spectroscopic missions such as WSO-UV [43] or CUTE [18].

The newly emergent detector architecture is that of CMOS devices. The only confirmed UV flight mission they have been baselined on at this time is the ULTRASAT mission to fly in 2025, although they are being considered for the UVEX NASA MIDEX mission currently under study [31]. The devices employ pixels in a 5T-design, that offers dual gain capability enabling a high-dynamic range operation mode. When combined with other standard features for the CMOS architecture such as non-destructive reads, up-the-ramp sampling and the ability to window areas of the device, the number of observing modes is increased dramatically. Like CCDs the devices suffer from a sensitive dependence of dark current on operational temperatures, but unlike CCDs there is no charge transfer efficiency problem – typical operational temperatures are 200K. CMOS devices can also be doped to target specific passbands, as is illustrated in Fig. 6 for the ULTRASAT devices.

Fig. 6
figure 6

Shown are three QE scans of the same ULTRASAT test sensor. The measurements are performed in the wavelength range 220-300 nm and over a period of 3 months. The first two measurements are subject to large wavelength uncertainties shown by a black errorbar in the upper left. The last measurement is calibrated using a Holmium Didymium absorption line filter leading to 0.2 nm uncertainties on the measurement [5]

FUV filters are challenging to build, their transmittance is typically low (peak transmittance is below 20% for 10 nm passbands) and reaching out-of-band rejections below \(\sim 10^{-4}\) is not easy. Early in the 70’s, peak transmissions of \(\sim \) 15 % were achieved for a 9 nm passband filter at Ly\(\alpha \) using Al/MgF\(_{2}\) layers deposition on a LiF substrate [33, 34]. These values have not been improved significantly over the intervening years mainly because of the technical difficulties imposed by the micro-roughness of the MgF\(_{2}\) films, which propagate to the thin Aluminium films causing an increase in the absorption. These older FUV filters also exhibit some performance evolution over time as shown in Fig. 7 [37]. More recently, use of techniques such as atomic layer deposition (ALD) [28, 40] have improved the optical uniformity and layer deposition thickness control to offer the possibility of a new generation of FUV interference filters.

Fig. 7
figure 7

FUV filters implemented in the Ionosphere Photometer of the Feng Yun-3D meteorological satellite. Left: Transmittance as a function of wavelength for a filter peaked at 135.6 nm both fresh (with a short exposure to the atmosphere) and after storage of 5 weeks in a desiccator. Transmittance of the aged sample at 10\(^{\circ }\) and 16\(^{\circ }\) is also displayed. Right: Transmittance in logarithmic scale (after [37])

A different approach is followed in the filter set implemented in the instrument Advanced CameraSystem (ACS) on HST, where many step filters are implemented in the 115-175 nm range. This enables broad band (bandwidth 30-50 nm) imaging by combining the transmission of a suite of step filters with the spectral sensitivity of the detector; it is, however, affected by red-leak problems.

Most FUV mirrors and gratings are coated with a thin film of MgF\(_{2}\) to prevent oxidation, but which also sets an effective sensitivity cut-off below 115 nm, which is especially dramatic when MCP detectors using MgF\(_{2}\) sealing windows are used. This fact has traditionally limited the UV range to above 115 nm (roughly above/below Ly\(\alpha \)) and although new technologies may enable the use of LiF to extend access below 115nm, most existing off the shelf UV reflective surfaces, especially those to be implemented in low cost missions, resort to using MgF\(_{2}\) for coating and sealing.

3.2 Environmental constraints

Another set of constraints to be considered is the sky background and the in-orbit environmental conditions; the UV background below 180 nm is roughly 4 orders of magnitude weaker than at optical wavelengths, however the upper layers of the Earth’s atmosphere produce a few, but very strong, emission lines of oxygen and hydrogen that can severely pollute UV spectra (see Fig. 8). However, astronomical observations from high earth orbit (HEO) satellites are not significantly affected by these lines unless the observing line of sight gets too close to the Earth limb. Observations from low earth orbit (LEO) satellites can be severely affected, in particular by the Lyman-\(\alpha \) transition of hydrogen at 122 nm and the OI triplet resonance transi+ons at 130.217, 130.486, and 130.603 nm.

Fig. 8
figure 8

Sky background intensity. The zodiacal contribution corresponds to m\(_{V}\) = 22.1 arcsec\(^{-2}\). The earthshine is for a target which is 38\(^{o}\) from the limb of the sunlit Earth. The geocoronal airglow line intensities are plotted at “average” intensities (https://hst-docs.stsci.edu/stisihb/chapter-6-exposure-time-calculations/6-5-detector-and-sky-backgrounds)

3.3 Interstellar extinction

The shape of the interstellar extinction curve can be modelled by a set of polynomial fits that extend from the far UV to the infrared using as free parameter \(R_{V} = A_{V}/E(B-V)\) [20]. The curve allows a simple parametrization in the infrared that extends smoothly into the optical range and is broken in the UV range by the presence of a strong absorption band (the so-called UV bump) at 225 nm (see Fig. 9). Five coefficients are used for the mathematical representation of the extinction law in the UV which is parametrized as,

$$\begin{aligned} k(\lambda - V) = E(\lambda - V)/E(B-V) = c_{1} + c_{2}x +c_{3} D(x,x_{0},\gamma ) \end{aligned}$$
(1)

with \(x=1/\lambda (\mu m)\) and,

$$\begin{aligned} D(x,x_{0},\gamma ) = \frac{x^{2}}{(x^{2}-{x_{0}^{2}})^{2}+x^{2}\gamma ^{2}} \end{aligned}$$
(2)

Parameters \(c_{1}, c_{2}, c_{3}, x_{0}\) and \(\gamma \) are constants that depend on the specific line of sight. The area of the bump is given by \(A_{\text {bump}} = \pi c_{3}/(2 \gamma )\) and its maximum intensity by \(I_{\text {bump}} = c_{3}/ \gamma ^{2}\). The width of the bump varies considerably with the line of sight but its central wavelength remains stable [19]. Originally, it was thought that the bump was produced by small graphite particles however, variations in the graphite grain shape and size should produce variations also in the central wavelength, \(x_{0}\) [17]. Nowadays, polycyclic-aromatic-hydrocarbons (PAHs) are thought to be the dominant component (see the review by [16] for more details).

Fig. 9
figure 9

A sample of extinnction curves based on the models CCM89 [12], GCC09 [24] and G16 [25], with variable \(R_V\) and mixture parameter \(f_A\). The filter set described in Section 4 fully samples the variability of the extinction curve in a wide variety of environments

The GALEX filter set was defined to compensate for the average galactic extinction. However, some small missions are now being specifically designed to study the distribution and properties of the interstellar dust in the Galaxy, rather than avoid it.

3.4 Other considerations

The density of spectral lines increases rapidly with photon energy, however any attempt to define the photometric system based on binning the UV range into 3-5 energy bins does not do a good job of reproducing the near UV continuum, and therefore hampers the definition of bands that can be used for the study of the UV extinction bump.

Table 2 UV photometric bands proposed as standards

Finally, since GALEX has provided the most extensive survey of the sky at UV wavelengths, it is a desirable feature of any new photometric system that the GALEX FUV and NUV bands should be included. In addition, extending the system up to the atmospheric cut-off at 350 nm is also highly desirable.

4 The photometric system

Based on the criteria exposed in Section 3, the UVA WG proposed a photometric system that consisted of three NUV bands NUV1 (GALEX NUV blue edge to 210 nm), NUV2 (210 nm - 235 nm), and NUV3 (235 nm - 275 nm); the GALEX FUV band; and an additional set of two to three bands to be later defined after consultation with the UV community, which would cover the 90-140 nm spectral range. Feedback from the community was then solicited. A questionnaire was distributed through the International Astronomical Union network, via the website pages belonging to the UVA-WG. Also, a general mailing to the registered members of the global Network for Ultraviolet Astronomy (gnuva.net) was issued; the feedback from this poll is summarized in Appendix. The results from the poll, together with the deliberations of the UVA-WG, were used to define the proposed list of filters that are summarized in Table 2.

Fig. 10
figure 10

The IAU-recommended UV bands. Some of them, UV2, UV3, UV6 and UV7, are already in use since they come from the Hubble instruments or from GALEX. For the new bands, simple (unrealistic) boxcar functions have been used with transmittances similar to the rest of the bands. See Table 2 for a summary

To visualize the characteristics of the system, the proposed UV1-UV7 magnitudes have been computed for the Hubble spectrophotometric standards; the UV bands are plotted in Fig. 10 and color-color diagrams for these 45 sources are displayed in Fig. 11.

Fig. 11
figure 11

Color-color diagrams for the UV spectrophotometric standards (red circles: white dwarfs; asterisks: A-type stars; black crosses: other types)

Fig. 12
figure 12

SPARCS UV filters probe key spectral regions important for both M dwarf non-thermal emission and exoplanet atmospheric molecules. Top: UV emission from M dwarfs atmosphere. Bottom: Cross section to photodissociation by UV radiation of relevant atmospheric molecules. The spectral coverage of the SPARCS UV filters (S-FUV, S-MUV, S-NUV) is shown in both panels

5 Example of implementation for Smallsats and Cubesats

The Star-Planet Activity Research Cubesat (SPARCS, [1]) is one of a few CubeSats currently under development for astronomical imaging in the ultraviolet. The key scientific objective of the mission is to monitor the high-energy radiation environment of the habitable zone exoplanets around M Dwarfs. Earth-like planets are easier to find around low mass stars and the scientific community is investing significant efforts to detect them. However, unlike solar-type stars, M dwarfs stay active with high emission levels and frequent flares throughout their lives [42]. The effects of sustained high levels of stellar activity on planetary atmospheres have not been studied since UV flare rates and energies across time are not well-known. Yet, we can expect that the increased UV emission and associated particle flux will have dramatic effects on a planet’s atmosphere (e.g., [32, 41]). The UV emission probed by SPARCS can, for instance, photodissociate important diagnostic molecules in a planetary atmosphere, such as water (H\(_{2}\)O), ozone (O\(_{3}\)), sulfur dioxide (SO\(_{2}\), a signature of volcanic activity), and ammonia (NH\(_{3}\), an important source of the nitrogen required to build amino acids) (Fig. 12, lower panel).

The transmittance of the filters (including the contribution from the detector spectral sensitivity) is shown in Fig. 13. The filter S-FUV is slightly shifted with respect to UV3 (GALEX FUV) to optimize the sensitivity to the CIV and He II lines. The filter S-NUV is similar to UV6 and the S-MUV is the sum of filters UV4+UV5.

SPARCS bands were defined for a very specific scientific purpose, and yet they are very close to the UV1-UV7 system proposed in this report. Moreover, given that the underlying spectral energy distribution of the sources is known (M-type stars), SPARCS magnitudes could easily be converted into the standard UV1-UV7 photometric system.

Fig. 13
figure 13

SPARCS throughput in the S-FUV, S-MUV and S-NUV bands

6 Summary and conclusions

Along with an overview of the astronomical instrumentation used to carry out UV photometry, this article presents the standard photometric system for UV astronomy approved by the IAU during the General Assembly in 2021, that should to be regarded as a tool for homogenizing photometry as part of the post-processing of the data. Its implementation is feasible because many missions and researchers have independently defined filters for their science that are rather similar (see Fig. 1), so translating them into the IAU standard system is straighforward. The implementation of such a system is crucial for the efficient and transparent use of the large wealth of data that is likely to be acquired in the near future.

The photometric system proposed in Section 4 cannot be implemented in terms of the optical description (transmission curves) of filters. The reflectivity of the coatings and the sensitivity of the detectors vary significantly across the UV spectral range; as shown in Fig. 13, the performance of a UV instrument depends on the combined contributions of all these components. As a consequence, the implementation of the system needs to be done “a posteriori” by post-processing the data from the individual missions into the standard system. The methods to define this standardization constitute the current core of the activity of the UVA WG. The computational resources are already available and the wealth of information in the astronomical archives will certainly aid in this process.

This type of activity fulfills one of IAU’s fundamental roles: to define standards of reference for information exchange. The fundamentals of the scientific method require the ability to test results by independent researchers which requires the definition of a clear and accessible framework for the interpretation of the data.

Finally, we would like to emphasize that there are currently several UV missions in definition, each with a different set of filters, and it would be very convenient to have a common framework for broad band photometry in all of the them.