ULYSSES
Ulysses HISCALE Data Analysis Handbook
4.8.1 Preflight Calibration with Electron Beams (continued)
Figure 4.60 LAN2B B detector electron detection efficiency, energy = 40 keV
Figure 4.61 LAN2B B detector electron detection efficiency, energy = 100 keV
Figure 4.62 LAN2B angular location of B peak efficiency
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