STEREO Mission Nick Chrissotimos NASA GSFC STEREO Project Manager SWG May 2, 2005
Mission Description Mission Objectives: 2 -year mission to measure the causes and mechanisms of CME initiation and characterization of their propagation through the heliosphere. 1 -year extended data analysis. Organizations: NASA GSFC, JHU/APL, Naval Research Laboratory, University of California at Berkeley, University of New Hampshire, University of Minnesota, Observatoire de Paris. Mission Description: Two functionally identical spacecraft in heliocentric orbits at 1 AU (22°/yr drift from Earth orbit leading/lagging configuration). Each Observatory: Volume: Dry Mass: Power: 1. 2 w x 2. 0 l x 1. 5 h meters A: 535 kg B: 561 kg 509 W (EOL) Launch: To be launched from KSC on a Delta 2925 -10 L. Website: http: //stereo. gsfc. nasa. gov SWG May 2, 2005 2
Observatory Configuration SWG May 2, 2005 3
Observatories Stacked in the Launch Vehicle Fairing Ahead (“A”) Observatory Behind (“B”) Observatory Delta II 3 Stage SWG May 2, 2005 4
Launch Vehicle SWG May 2, 2005 5
Launch Timeline SWG May 2, 2005 6
Coverage Maps March 2006 February 2006 April 2006 SWG May 2, 2005 7
SWG May 2, 2005 8
SWG May 2, 2005 9
Separation and Solar Array Deployments SWG May 2, 2005 10
Spacecraft B and A SWG May 2, 2005 11
Spacecraft A SWG May 2, 2005 12
IMPACT IDPU Mechanically Integrated SWG May 2, 2005 13