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 | 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 Area | Primary 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 Capabilities | Imaging Elements | F062 (R), F087 (z), F106 (Y), F129 (J), |
|
Sensitivity | 27.5 mag (AB) at 5-sigma in 1 hour at ~1.5 microns | ||
Spectroscopic Capabilities | Dispersive Elements | P120 (prism), G150 (grism) | |
Sensitivity | 21.5 & 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.
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 Meters | 45' x 23' 0.28 sq deg | 0.11''/pixel | 0.5 to 2.3 microns |
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 | F087 | F106 | F129 | F146 | F158 | F184 | F213 | |
---|---|---|---|---|---|---|---|---|
Ground Equivalent | R | Z | Y | J | H | H/K | Ks | |
Wavelength (microns) | 0.48 - 0.76 | 0.76 - 0.98 | 0.93 - 1.19 | 1.13 - 1.45 | 0.93 - 2.00 | 1.38 - 1.77 | 1.68 - 2.00 | 1.95 - 2.30 |
Sensitivity | 27.9 | 27.6 | 27.5 | 27.5 | 27.9 | 27.4 | 26.7 | 25.4 |
PSF Half-Light Radius | 120 | 130 | 130 | 140 |
Table of Wide Field Instrument Slitless Spectroscopy & Sensitivity
Element Name | Wavelength (microns) | Continuum Sensitivity (AB Mag 5-sigma/pix in 1 hour | Spectral Resolution | |
---|---|---|---|---|
Grism | P120 | 1.00 - 1.93 | 21.4 at 1.5 microns | 461 |
Prism | G150 | 0.75 - 1.80 | 23.5 at 1.5 microns | 80 - 180 |
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 | 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 | 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 | Not yet Document on RDox |
Noise | 5 electrons correlated noise floor read noise below below 20 electrons | Not yet Document on RDox |
For additional questions not answered in this article, please contact the Roman Help Desk at STScI.