HPDE.io

Low-Energy Electrons (LEE)

ResourceID
spase://SMWG/Instrument/AE-D/LEE

Description

This experiment provided direct measurements of the energy input into the upper
atmosphere due to electrons and protons in the energy range of 0.2 to 25 keV. The experiment
acquired differential measurements of the energy influx and angular distribution. There were
two detectors measuring electrons and protons from 0.2 to 25 keV in 16 logarithmically spaced
steps, and one detector measuring 5 keV electrons continuously. Each detector consisted of a
cylindrical electrostatic analyzer for species and energy selection, and a Spiraltron electron
multiplier for particle detection. Energy distributions were obtained by applying different
fixed or stepped voltages to the deflection plates. Distributions in angle were measured using
the spacecraft spin and the analyzers' positions on the spacecraft. In the despun modes,
measurements were obtained at 45 deg to the spacecraft equator, and radially away from the
earth. Detector look angles were chosen to give optimum magnetic pitch-angle coverage when the
spacecraft was moving either poleward or equatorward. All detectors were identical in construction
and used 1- x 6-mm entrance apertures. Counts were accumulated over 55.7 ms and read out each
main telemetry frame (62.5 ms). The two stepped detectors moved one energy step once each main
frame with the same accumulation time, requiring about 1 s for a complete cycle of steps. More
complete details of this experiment may be found in
R. A. Hoffman et al., Radio Sci., v. 8, n. 4, p. 393, 1973. NSSDC has all the useful data that
exist from this investigation.

View XML | View JSON | Edit

Details

Version:2.0.0

Instrument

ResourceID
spase://SMWG/Instrument/AE-D/LEE
ResourceHeader
ResourceName
Low-Energy Electrons (LEE)
AlternateName
LEE
ReleaseDate
2019-05-05 12:34:56Z
Description

This experiment provided direct measurements of the energy input into the upper
atmosphere due to electrons and protons in the energy range of 0.2 to 25 keV. The experiment
acquired differential measurements of the energy influx and angular distribution. There were
two detectors measuring electrons and protons from 0.2 to 25 keV in 16 logarithmically spaced
steps, and one detector measuring 5 keV electrons continuously. Each detector consisted of a
cylindrical electrostatic analyzer for species and energy selection, and a Spiraltron electron
multiplier for particle detection. Energy distributions were obtained by applying different
fixed or stepped voltages to the deflection plates. Distributions in angle were measured using
the spacecraft spin and the analyzers' positions on the spacecraft. In the despun modes,
measurements were obtained at 45 deg to the spacecraft equator, and radially away from the
earth. Detector look angles were chosen to give optimum magnetic pitch-angle coverage when the
spacecraft was moving either poleward or equatorward. All detectors were identical in construction
and used 1- x 6-mm entrance apertures. Counts were accumulated over 55.7 ms and read out each
main telemetry frame (62.5 ms). The two stepped detectors moved one energy step once each main
frame with the same accumulation time, requiring about 1 s for a complete cycle of steps. More
complete details of this experiment may be found in
R. A. Hoffman et al., Radio Sci., v. 8, n. 4, p. 393, 1973. NSSDC has all the useful data that
exist from this investigation.

Contacts
RolePersonStartDateStopDateNote
1.PrincipalInvestigatorspase://SMWG/Person/Robert.A.Hoffman
InformationURL
Name
NSSDC's Master Catalog
URL
Description

Information about the Low-Energy Electrons (LEE) experiment on the AE-D mission.

InformationURL
Name
Radio Science Journal Article
URL
Description

Detailed information about the Low-Energy Electrons experiment on the AE-D mission.

InstrumentType
ElectrostaticAnalyser
InvestigationName
Low-Energy Electrons (LEE) on AE-D
ObservatoryID