ULYSSES
Ulysses HISCALE Data Analysis Handbook
4.8.1 Preflight Calibration with Electron Beams (continued)
Figure 4.66 Electron detection efficiency 30° CCW
Figure 4.67 Electron detection efficiency 20° CCW
Figure 4.68 Electron detection efficiency 10° CCW
Figure 4.69 Electron detection efficiency 0°
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Return to Ulysses HISCALE Data Analysis Handbook Table of Contents
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