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Spacecraft

OVERVIEW

The two STEREO spacecraft will be built by Johns Hopkins University Applied Physics Laboratory (Laurel, MD).

The two STEREO spacecraft are identical and designed for a 2 year mission. Most spacecraft operations (antenna pointing control, momentum management, power management, and thermal management) are autonomous.

Relevance

STEREO's relevance to human life on Earth and the domestication of space provides a natural platform for enhancing the scientific and technological literacy of children and adults nationwide. Specifically, the spectacular imagery of the Sun and inner heliosphere to be obtained with SECCHI will provide unique opportunities for education and public outreach.

Mechanism Statistics

SECCHI Shutter Mechanism Spin Times

Polarizer Spin Times

as of 2017/12/21 (COR 1-B 2014/09/30)

Note: For Feb.-Oct. 2012, the COR 1-B polarizer data points are a change from previous. A CCW test is done before the CW test. For previous CCW tests back in 2007, the mechanisms were first spun CW, then CCW. For 2012 the order was reversed. This change was implemented for all polarizers starting 2012/04/17, and then discontinued in October 2012.

Anomaly Reports

EUVI-A Quadrant Selector Anomaly

A change in brightness was noted for some EUVI 171 Angstrom images starting in 2011. This was determined to be due to a change in the required mechanism delay setting, which fixed the problem. However, the problem persisted on a few occasions when the delay setting was set to the old value: