march 19, 2002 slac
DESCRIPTION
Face-to-Face IDT Meeting Session 3 Characterization of the South Atlantic Anomaly for the LAT S. W. Digel. March 19, 2002 SLAC. Origin of the South Atlantic Anomaly. - PowerPoint PPT PresentationTRANSCRIPT
GLAST LAT Project Face-to-Face IDT Meeting, March 19–20, 2001
Session 1 1
Face-to-Face IDT Meeting Session 3Face-to-Face IDT Meeting Session 3Characterization of the South Atlantic Characterization of the South Atlantic
Anomaly for the LAT Anomaly for the LAT
S. W. DigelS. W. Digel
March 19, 2002
SLAC
GLAST LAT Project Face-to-Face IDT Meeting, March 19–20, 2001
Session 1 2
Origin of the South Atlantic AnomalyOrigin of the South Atlantic Anomaly
• Offset and tilt of the magnetic axis with respect to the rotation axis permits the intense trapped radiation (circulating on magnetic field lines) to reach relatively low altitudes in a large region more or less centered on the south Atlantic
http://www.estec.esa.nl/wmwww/wma/rad_env.html
GLAST LAT Project Face-to-Face IDT Meeting, March 19–20, 2001
Session 1 3
General Issues for Operation in the SAAGeneral Issues for Operation in the SAA
• Radiation damage to detectors, SEUs, latchups• Charging of spacecraft, instruments – arcing, overcurrent
damage to high-voltage devices• For LAT: The high rate of triggers on charged particles within
the SAA is likely to saturate the data acquisition system (large deadtime), and extracting useful celestial photons may be problematic anyway.
GLAST LAT Project Face-to-Face IDT Meeting, March 19–20, 2001
Session 1 4
Options for Coping with the SAAOptions for Coping with the SAA
• SAA task force met last May• Options defined
1. GPS and a map of boundary to have LAT turn itself (i.e., ACD high voltage) off and on
2. Stored (uploaded) commands to turn off and on
3. ACD rate (possibly in a time) to define turn off/on times
4. Dedicated SAA detector to do the same thing
5. Self-protect the components
• Option 2 is a given; ≥1 more for desired reliability [may not be clear what the impact on the instrument would be of being on during SAA passage]
GLAST LAT Project Face-to-Face IDT Meeting, March 19–20, 2001
Session 1 5
More OptionsMore Options
• Fly under (or around) the SAA
AP8MIN, >1 proton cm-2 s-1 (>1 MeV)
6°
30°
Inclination of orbit
18°Nominal altitude, inclination of GLAST
Rep
rese
nta
tive
GLAST LAT Project Face-to-Face IDT Meeting, March 19–20, 2001
Session 1 6
Radiation Environment of the SAARadiation Environment of the SAA
• Modeling the SAA – AP8 & AE8 models
• Fluxes are really anisotropic
• SAA changes size and is moving (~0.3°/yr to the west)
Trapped Protons
Trapped Electrons
Differential Intensities at Peak