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Explorer: TESS (Astro-EX 1)

TESS (Astro-EX 1) [MIT]

TESS (Transiting Exoplanet Survey Satellite) will use an array of telescopes to perform an all-sky survey to discover transiting exoplanets ranging from Earth-sized to gas giants, in orbit around the nearest and brightest stars in the sky. Its goal is to identify terrestrial planets in the habitable zones of nearby stars. Its principal investigator is George Ricker of the Massachusetts Institute of Technology in Cambridge.

TESS team partners include the MIT Kavli Institute for Astrophysics and Space Research (MKI) and MIT Lincoln Laboratory; NASA’s Goddard Spaceflight Center; Orbital Sciences Corporation; NASA’s Ames Research Center; the Harvard-Smithsonian Center for Astrophysics; The Aerospace Corporation; and the Space Telescope Science Institute.

Unlike Kepler, which looks at a single region of the sky, TESS will perform an all-sky survey, focusing on stars within about 200 light-years of the Earth and identifying nearby exoplanets for followup observations.

TESS will launch by 2017 into a 2 to 1 lunar resonance highly elliptical orbit of 17 × 59 RE (Earth radii) by using a perigee kick motor and a lunar flyby, operating for at least two years (starting at the conclusion of a 2 month ascent and commissioning phase) with consumables designed for a 4 year mission life. Equipped with four wide-field cameras, the spacecraft would be able to observe potentially hundreds of thousands of stars, looking for those telltale periodic dips in brightness caused by transiting exoplanets.

Orbital was selected to provide a LEOStar-2 based bus.

TESS was baselined with Athena-2c or Taurus-3210, both with additional Star-37FM kick motor. The baselined launch site is Cape Canaveral. Also Antares and Falcon-9 v1.2 are considered. In December 2014, a Falcon-9 v1.2 was selected to put TESS into orbit.

Nation: USA
Type / Application: Astronomy, visible
Operator: MIT for NASA
Contractors: Orbital Sciences Corporation (OSC)
Configuration: LEOStar-2
Propulsion: ?
Power: 2 deployable solar arrays, batteries
Lifetime: 2 years
Mass: 325 kg
Orbit: 17 RE × 59 RE
Satellite COSPAR Date LS Launch Vehicle Remarks
TESS (Astro-EX 1) - 2018 CC Falcon-9 v1.2
Further Astro-EX missions: