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Ulysses HISCALE Data Analysis Handbook

 

 

4.8 Calibrations (continued)

 

4.8.1 Preflight Calibration with Electron Beams (continued)

 

Memo #2: Additional Data Presentation to Solar-Polar LAN-2B Electron Calibration Report

 

Document Source: J. W. Kohl (LAN-041-80)
Date: October 2, 1980

 

By request of L. Lanzerotti, the data contained in the report “Calibration of Solar-Polar LAN-2B Flight Unit at NASA/GSFC with Laboratory Electronics Using Low Energy Electrons,” August 1980, has been presented in a different format.

 

Attached are graphs indicating the electron detection efficiency for beam targets in the Y = 0 plane (coordinate systems are those described in the above mentioned report). The data is presented as efficiency as a function of target position along the Z axis for a constant beam entrance angle. Each curve is identified as to electron energy.

 

Note that the 20 keV electron efficiency has been modified for the low level discriminator cut-off efficiency, so that what is presented in the figures are the true efficiencies.

 

 

 

Next: Chapter 4.8.2 Preflight Calibrations with Ion Beams

 

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