Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.



WFIRST (Wide-Field Infrared Survey Telescope) is a planned NASA observatory designed to perform wide-field imaging and slitless spectroscopic surveys of the near infrared (NIR) sky.

The current Astrophysics Focused Telescope Assets (AFTA) design of the mission makes use of an existing 2.4 m telescope, inherited from the defunct FIA-Optical reconnaissance satellite program, to enhance sensitivity and imaging performance. WFIRST-AFTA will settle essential questions in both exoplanet and dark energy research and will advance topics ranging from galaxy evolution to the study of objects within the Galaxy and within the Solar System. It is the top-ranked large space mission in the New Worlds, New Horizon (NWNH) Decadal Survey of Astronomy and Astrophysics. The main instrument is a wide-field multi-filter NIR imager and spectrometer. With the 2.4 m telescope, a coronagraph instrument has been added to the payload for direct imaging of exoplanets and debris disks.

The WFIRST-AFTA Design Reference Mission (DRM) uses existing 2.4-meter telescope hardware, along with heritage instrument, spacecraft, and ground system architectures and hardware to meet the WFIRST-AFTA science requirements.

The payload features a telescope with a 2.4-meter aperture and on-axis secondary mirror, which feeds two different instrument volumes containing the wide field and coronagraph instruments. The telescope hardware was built by ITT/Exelis under contract to another agency and is being made available to NASA. The telescope is a space flight qualified 2.4-meter, obscured two-mirror system. Repurposing modifications will include conversion to a three-mirror anastigmat (TMA) optical configuration to enable a wide field-of-view instrument and replacements for hardware that was not provided to NASA. This existing hardware significantly reduces the development risk of the WFIRST-AFTA payload.

The wide field instrument provides the wide-field imaging and slitless spectroscopic capabilities required to perform the Dark Energy, Exoplanet Microlensing, and NIR surveys while the coronagraph instrument supports the Exoplanet high contrast imaging and spectroscopicy science. The wide field instrument includes two channels, a wide field channel and an integral field unit (IFU) spectrograph channel. The wide field channel includes three mirrors (two folds and a tertiary) and a filter/grism wheel to provide an imaging mode covering 0.76 2.0 m and a spectroscopy mode covering 1.35 1.95 m. The wide field focal plane uses 4k × 4k HgCdTe detectors with 10 m pixels. The HgCdTe detectors are arranged in a 6×3 array, providing an active area of 0.281 deg2. The IFU channel uses an image slicer and spectrograph to provide individual spectra of each 0.15"wide slice covering the 0.6 2.0 m spectral range over a 3.00 × 3.15 arcsec field. The instrument provides a sharp point spread function, precision photometry, and stable observations for implementing the Dark Energy, Exoplanet Microlensing, and NIR surveys.

In the current DRM, WFIRST-AFTA is deployed in a 28.5 inclined geosynchronous orbit and will operate for a minimum of 6 years. The geosynchronous orbit allows continuous downlink to the ground, enabling a high science data rate. WFIRST-AFTA is designed to be robotically serviceable, should a future robotic servicing capability be deployed in geosynchronous orbit. Serviceability is implemented at a module level, i.e. an entire instrument or a spacecraft module containing multiple electronics boxes. The modularity will also be a benefit during integration and test of the observatory. On the payload side, an instrument carrier was designed to attach to the existing telescope metering structure interfaces and provide volumes for two instrument modules. The instrument carrier provides mechanical latches, with design heritage from HST, to interface the instrument modules to the carrier, contains harness to route power and data between the spacecraft and the instrument modules, and provides thermal isolation between the two instrument volumes. Each of the spacecraft modules includes a kinematic Module Restraint System based on the Multimission Modular Spacecraft design, which was proven during the on-orbit module change out on the Solar Maximum Mission Repair Mission.

The mission is baselined for a launch in 2024 on a Delta-4H (upg.) rocket.

Nation: USA
Type / Application: Astronomy (IR)
Operator: NASA
Equipment: 2.4 m telescope
Power: Solar cells, batteries
Lifetime: 6 years
Orbit: GEO, 28
Satellite COSPAR Date LS Launch Vehicle Remarks
WFIRST - 2024 CC SLC-37B Delta-4H (upg.) (baselined)