WFI Quick Reference

This article provides quick at-a-glance information about the capabilities of the Wide Field Instrument (WFI) and places these in context of other major astronomical projects. 





Key Information for Using Roman's WFI 

The Wide Field Instrument (WFI) is a one-of-a-kind instrument and is a key component to the survey capabilities of Roman. The Table of Key Parameters for Roman's WFI provides quick at-a-glance information about Roman, the WFI, and its capabilities. Links in the Table provide direct paths to resources that may be valuable. For information on the data from WFI and how it will be made available to the community, please see the Data Handbook.

Table of Key Information for Roman's WFI 



Characteristic

Reference Values

(lightbulb) Learn More

Roman as an Observatory

Target Availability

Field of Regard

59% of the sky is available at one time

Slew & Settle Times

less than 2.5 minutes for slews under 5 degrees
Collecting AreaPrimary Mirror Diameter

2.4 m

Collecting Area

4.5 m2

Capabilities of the Wide Field Instrument 

Basic Properties

Field-of-View

0.28 sq degree

Wavelength Range

0.5 to 2.3 microns

Plate Scale

0.11''/pixel
Imaging CapabilitiesImaging Elements

F062 (R), F087 (z), F106 (Y), F129 (J), 
F146 (wide), F158 (H), F184 (H/K), F213 (Ks)

Sensitivity 27.5 mag (AB)
at 5-sigma in 1 hour at ~1.5 microns
Spectroscopic CapabilitiesDispersive ElementsP120 (prism), G150 (grism)
Sensitivity21.5 & 23.5 mag (AB)
at 5-sigma in 1 hour at ~1.5 microns



Observatory Capabilities 

The Roman spacecraft will be maintained in a Sun-Earth L2 orbit. Observing zones are defined such that the solar panels can provide maximum power, and for avoidance of the bright Earth and Moon. The Field of Regard (FOR) provides access to roughly 40% of the sky each day, and the full sky is available over the 5-year primary mission. The spacecraft slew and settle rates allow for the efficient execution of large surveys.

Field of Regard

As shown in the Figure of the Field of Regard and Slew + Settle Times for Roman, the observing zone is described by: a pitch of 54 degrees to 126 degrees from the Sun line, 360 degrees of yaw around the Sun line, and a +/- 15 degrees about the line of sight off the max power role angle. Keep-Out Zones are those areas of pitch less than 54 degrees from the Sun line and greater than 126 degrees from the Sun line. There are also minor sporadic constraints on pointing due to the Earth and Moon line-of-sight avoidance areas. More detailed information on target visibility and available roll angles can be found at the GSFC Field, Slew, and Roll article, with a detailed roll angle table available for more precise applications.

Slew and Settle Times

As shown in the Figure of the Field of Regard and Slew + Settle Times for Roman, the observatory is designed for quick moves for efficient sky mapping. Moves of 5 degrees or less can be completed in under 3 minutes. A more detailed Slew Table is provided by GSFC. Small slews, like those in a 5-point dither, would be of only a few seconds with a 10 second settle time. 


Figures of the Field of Regard and Slew + Settle Times for Roman



(a) The Field of Regard (FOR) for Roman as defined around the Sun-line from its orbit at L2. The line-of-sight to the Galactic Bulge, labelled as the grey circle with the text "GB", is available to the telescope twice annually. The Keep-Out Zone is also indicated in blue. These features of the telescope determine what parts of the sky the observatory has access to at any given date. (b) The Roman observatory is optimized for surveys with relatively fast slew+settle times for small and large moves. (Image Source: Roman at GSFC)

How to Find more Detailed Information

The Goddard Space Flight Center provides a Field, Slew, and Roll article, with a detailed roll angle table available for more precise applications and a very detailed machine readable Slew Table is provided. The pySIAF for Roman for Roman article in the Simulation Tools Handbook provides software access to relevant coordinate transformations. 



Capabilities of WFI on Roman 

The Wide Field Instrument (WFI) of the Roman Space Telescope has both imaging and slitless spectroscopy capabilities, and a large field of view. The Table of Wide Field Instrument Capabilities summarizes the at-a-glance information. The active area on the sky is 0.281 square degrees, roughly 100 times the area covered by HST/ACS or JWST/NIRCam, and 200 times that of WFC3/IR. The WFI has 18 H4RG-10 (HgCdTe) 4096 pixel by 4096 pixel detectors for over 300 million active pixels with a plate scale of 0.11 arcsec/pix, similar to WFC3/IR. WFI is sensitive to wavelengths from 0.5 to 2.3 microns. The imaging capabilities of the Hubble Space Telescope, Roman Space Telescope, and JWST are compared in the Figure Comparing the Hubble, Roman, and James Webb Space Telescopes. The WFI Design article provides a detailed description of the full instrument and its key subsystems. 

How to Find more Detailed Information

The WFI Design article provides a detailed description of the full instrument and its key subsystems. 

Table of Wide Field Instrument Capabilities 

Telescope Aperture

Field of View 

Pixel Scale

Wavelength Range

2.4 Meters45' x 23' 
0.28 sq deg
0.11''/pixel0.5 to 2.3 microns

Figure Comparing the Hubble, Roman, and James Webb Space Telescopes 

This infographic shows the complementary capabilities of select instruments on three of NASA's flagship missions: the Hubble Space Telescope and the currently under development Nancy Grace Roman Space Telescope and James Webb Space Telescope. Hubble views the cosmos in near-infrared, visible, and ultraviolet light, providing high-resolution views of individual objects. The Roman Space Telescope will expand on Hubble’s legacy of visible to near-infrared observations with its significantly larger field of view. Roman is uniquely able to create enormous panoramas of the universe with more-or-less the same spatial resolution as Hubble. During the span of Roman's mission, Webb will be conducting the highest-resolution visible, near-infrared, and infrared observations ever feasible. With the largest aperture of the three observatories, Webb will peer to the farthest stretches of space, but with a narrower field of view. 

(Image Credit: NASA's Goddard Space Flight Center; Link to Original)



WFI Optical Elements and Sensitivity

The WFI provides 8 filters, including 7 filters isolating various broad bands (corresponding to the ground-based filters of R, z, Y, J, H, H/K, Ks), and one wide filter (F146). The Table of WFI Imaging Filters & Sensitivity provides the wavelength ranges, the 5-sigma sensitivity for a 1-hour exposure time, and the half-light radius for the PSF. WFI will have no narrow band filters. Two dispersers can be used for slitless multi-object spectroscopy and these are the prism (P120) and grism (G150). The Table of WFI Slitless Spectroscopy & Sensitivity summarizes the wavelength ranges, resolution, and the 5-sigma continuum sensitivity for a 1-hour exposure time. The Figures Contextualizing the Survey Grasp and Sensitivity of Roman place the capabilities of the WFI into the context of other wide-field observatories (Rubin and Euclid) as well as comparing against other large-scale surveys in the near-infrared. 

How to Find more Detailed Information

The Optical Elements article in the WFI Imaging Mode User Guide provides significantly more detail on the wavelength coverage and throughput of the optical elements. In the Simulation Tools Handbook, the Synphot for Roman article describes how to access the response functions using python. The direct response function tables, as currently characterized, are available with the Roman Space Telescope Reference Information that is maintained by NASA Goddard Space Flight Center.


Table of Wide Field Instrument Imaging Filters & Sensitivity 


F062 F087F106F129F146F158F184F213
Ground EquivalentRZYJ
HH/KKs
Wavelength (microns)0.48 - 0.760.76 - 0.980.93 - 1.191.13 - 1.450.93 - 2.001.38 - 1.771.68 - 2.00

1.95 - 2.30

Sensitivity
(5-sigma AB mag in 1 hour)

27.927.627.527.527.927.426.725.4

PSF Half-Light Radius
(milliarcsec)



120130
130140

Table of Wide Field Instrument Slitless Spectroscopy & Sensitivity 


Element NameWavelength 
(microns)

Continuum Sensitivity

(AB Mag 5-sigma/pix in 1 hour

Spectral Resolution
GrismP1201.00 - 1.9321.4 at 1.5 microns461
PrismG1500.75 - 1.8023.5 at 1.5 microns80 - 180

Figures Contextualizing the Survey Grasp and Sensitivity of Roman 

The left panel displays the 5-sigma point source threshold in AB magnitudes against the filter wavelength for LSST (blue), Euclid (green), and Roman (red). Labels indicate the PSF half-light radius in units of milliarcsec. Corresponding data for Roman is in the Table of Wide Field Instrument Imaging Filters & Sensitivity. The right figure shows the survey grasp in sq. degrees per sq. arcseconds versus the flux sensitivity in milli-Janskys and compares Roman to 2MASS, WISE, UKIDSS, CFHTLS, Euclid, CANDLES, and the HUDF/IR for a subset of relevant filters. (Image Credit: NASA; Link to Originals; Note that some labels were made larger for readability in RDox)



WFI Detectors

The WFI mosaic plate assembly provides both fine guiding and science data readout. The array of 18 detectors (Teledyne H4RG-10; also known as Sensor Chip Assemblies or SCAs) covers 0.281 square degrees on the sky with 300 megapixels. To manage data volume, WFI employs both data compression and multi-accumulation (MA) readouts. The Table of Basic Detector Properties provides at-a-glance information about the Roman detectors. 

How to Find more Detailed Information

Further information regarding detector calibration and performance will be added in future releases of RDox.


Table of Basic Detector Properties 

Characteristic

Quick Reference Values(lightbulb) Learn More

Individual Detector Properties

Detector type

18 individual Teledyne H4RG-10 

Pixels are 10 x 10 microns

More Description is given in the WFI Design article.

Single Detector Pixel Dimensions

4096 x 4096 pixels total

4088 x 4088 pixels active

Single Detector on the Sky

450 x 450 arcsec

See the WFI Focal Plane In Context below.

Focal Plane Properties

Focal Plane Area 

300 Mega Pixels

See the WFI Focal Plane In Context below.

Focal Plane Array Area on Sky

0.320 square degrees (total)

0.281 square degrees (effective)

Detector Performance

Dark current

below 0.1 electrons/sec/pixel

(error)  Not yet Document on RDox

Quantum Efficiency

above 80% from 0.8 to 2.1 microns

above 60% from 0.6 to 0.8 microns

(error)  Not yet Document on RDox

Noise

5 electrons correlated noise floor

read noise below below 20 electrons

(error)  Not yet Document on RDox


The WFI Focal Plane in Context 


The first image shows the Focal Plane Array (FPA) for WFI that contains 18 Teledyne H4RG-10 with 4096 pixels by 4096 pixels (Image Credit: NASA/Chris Gunn; Link to Original). The second image places the WFI's wide-field-of-view in context of the Andromeda galaxy. WFI can image the main body of Andromeda in just a few pointings, surveying the galaxy nearly 1500 times faster was feasible with the Hubble Space Telescope. The footprint of WFI on the sky is similar to the area subtended by the full Moon, which is shown to scale in the upper right (Composite Image Credit: GSFC/SVS; Link to Original; Moon Image Credit: NASA/GSFC/ASU/Lunar Reconnaissance Orbiter; Background Sky Image Credit: Digitalized Sky Survey and R. Gendler). 





For additional questions not answered in this article, please contact the Roman Help Desk at STScI.




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