ULYSSES
Ulysses HISCALE Data Analysis Handbook
4.8.1 Preflight Calibration with Electron Beams (continued)
Figure 4.63 LAN2B B detector peak electron efficiency as f (energy)
Figure 4.64 Electron energy deposited in detector F
Figure 4.65 Electron detection efficiency of detector F LAN2B as f (energy)
Return to Chapter 4 Table of Contents
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