Wide-field Infrared Survey Explorer



NEWS:

21 Jun 2007 - WISE has passed its Mission Critical Design Review, held 18-21 June 2007 at UCLA.

13 Oct 2006 - WISE has been confirmed by NASA headquarters. The launch is scheduled for November 2009.

25 Aug 2004 - WISE has been selected by NASA as its next Medium-Class Explorer. With this decision the WISE mission will proceed into Phase B (Definition Phase). This phase will conclude with a preliminary design review in April 2005. Read the press release and visit our new public Web page.

29 April 2003 - WISE releases a simulated distribution of Brown Dwarfs in the Solar Neighborhood. These data and the viewer are available from our E/PO partner Hayden Planetarium at the American Museum of Natural History.

20 March 2003 - WISE has been selected for an extended Phase A study leading to a decision in 2004 on whether to proceed with the development of the mission. Read the NASA press release on the MidEx selection.


Science Objectives

WISE will provide an all-sky survey from 3.3 to 23 microns up to 1000 times more sensitive than the IRAS survey.

WISE will

Simulated WISE images.

Current WISE Status

This figure shows the 5 sigma point source sensitivities of WISE and previous or planned all-sky surveys. The planned wavelength range for the JWST is indicated. The dot size shows the planned sky coverage. GALEX is a small Explorer (SMEX) which was launched by NASA in 2003, SDSS is the groundbased Sloan Digital Sky Survey, DPOSS is the groundbased Digital Palomar Observatory Sky Survey, ASTRO-F is the Japanese satellite, renamed Akari after launch on 22 Feb 2006, and Planck is the European CMB mission to be launched in 2008 which also includes a good sub-mm survey capability.


Mission Overview

thumbnail of proposal cover page artwork

Science Payload

The single WISE instrument is a four-channel imager which will take overlapping snapshots of the sky. It includes:

Key Spacecraft Characteristics

Mass: 750 kg including contingency
Basic Design: Three-axis stabilized. Body-fixed solar arrays. Fixed high gain antenna.
Power: 2.4 m2 GaInP2/GaAs/Ge triple junction solar cells: 382 W EOL orbit average power; Li ion battery.
Telemetry: Ku-band to TDRSS during polar passages.
Data Rate: 23 GB per day (compressed)
Data Storage:    96 GB
Propulsion: None

Mission Management

PI: Edward L. (Ned) Wright, UCLA Physics & Astronomy
Co-I's: Science team
Project management: JPL
Spacecraft:    Ball Aerospace
Instrument: SDL
Detectors: DRS and Teledyne (formerly RSC)
Cryostat: Lockheed-Martin
Data analysis: IPAC
EPO: UC Berkeley Space Science Laboratory

Last modified 06 Sep 2007