Template:Infobox spaceflight

The Active Cavity Radiometer Irradiance Monitor Satellite, or ACRIMSAT is a dedicated satellite and instrument that was one of the 21 primary observational components of NASA's Earth Observing System program. ACRIMSAT was launched on 20 December 1999 from Vandenberg Air Force Base as the secondary payload on a Taurus rocket along with KOMPSAT. It was placed into a high inclination, 700 km. sun-synchronous orbit from which the ACRIM3 instrument monitored total solar irradiance (TSI).[1] Contact with the satellite was lost on 14 December 2013.[2]


ACRIM3 made measurements of the TSI since the start of its mission in April 2000. It extended the TSI measurement database begun by earlier ACRIM instruments on the NASA Solar Maximum Mission (ACRIM1: 1980-1989) and Upper Atmosphere Research Satellite (ACRIM2: 1991-2001).[citation needed]

ACRIMSAT/ACRIM3 tracked TSI during a 2004 transit of Venus and measured the 0.1% reduction in the solar intensity caused by the planet's shadow.[3] It also recorded data for the 2012 Transit of Venus.[4]

On 14 December 2013, ACRIMSAT went silent, with attempts to reestablish contact proving unsuccessful. The mostly likely cause has been attributed to the failure of aging batteries. The defunct spacecraft will remain in orbit for approximately 64 years before returning to Earth.[2]


Richard C. Willson is the principal investigator and leads the science team.[5] Willson designed the active cavity radiometer type of sensor used by self-calibrating satellite TSI monitoring experiments. The ACRIM3 instrument was a collaboration between Willson, original JPL/ACRIMSAT Project Manager Ronald Zenone and ACRIM3 Instrument Scientist Roger Helizon. The Mission is controlled using the ACRIMSAT tracking station at the Jet Propulsion Labs (JPL) Table Mountain Observatory in Southern California. Co-Investigators are: Nicola Scafetta (climate impact of solar variability), Hugh Hudson (solar physics)and Alexander Mordvinov (solar physics).


ACRIMSAT (international designator 1999-070B) is a spin-stabilized, single-purpose satellite constructed by Orbital Sciences Corporation. Its total cost, including the instrument, launch, ground station, operations and science team activities during its 14-year mission was less than $50 million.


External linksEdit

Template:Sun spacecraft

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