ULYSSES
Ulysses HISCALE Data Analysis Handbook
Chapter 4: Instrument
Details
4.4 Passband Data and Calculated Responses
Table 4.10 Composition Aperture (WART) parameters and logic
Figure 4.30 Composition aperture energy losses
Figure 4.31 Delta E versus E for composition aperture (WART)
Figure 4.32 WART channel definitions
| Absorber 2 | Absorber 3 | |
| Absorber Material | Silicon | Silicon |
| Thickness (microns) | 4.50 | 200.00 |
| RMS UNC (microns) | 0.10 | 2.00 |
| Max. Conical Half Ang. | 22.50 | 22.50 |
| Detector AMS Noise (keV) | 29.00 | 0.00 |
| Electronic Noise (keV) | 65.00 | 10.00 |
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Updated 8/8/19, Cameron Crane
QUICK FACTS
Manufacturer:
ESA provided the Ulysses spacecraft, NASA provided the power
supply, and various others provided its instruments.
Mission End Date: June 30, 2009
Destination: The inner heliosphere of the sun away from the ecliptic plane
Orbit: Elliptical orbit transversing the polar regions of the sun outside of the ecliptic plane
Mission End Date: June 30, 2009
Destination: The inner heliosphere of the sun away from the ecliptic plane
Orbit: Elliptical orbit transversing the polar regions of the sun outside of the ecliptic plane