ULYSSES In Space

 

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ULYSSES

Ulysses HISCALE Data Analysis Handbook

 

 

4.8 Calibrations

 

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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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