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ISS Floating Potential Measurement Unit (FPMU), Summary Parameter 1 s Data

ResourceID
spase://NASA/NumericalData/ISS/FPMU/PT1S

Description

International Space Station, ISS, Floating Potential Measurement Unit, FPMU, Ionosphere Summary Wide Langmuir Probe, WLP, Density and Narrow Langmuir Probe, NLP, Temperature Records 1 s Data. The Space Dynamics Laboratory, SDL, Utah State University, USU, developed the FPMU for the NASA Johnson Space Center. The FPMU was installed by ISS Crew Members during an Extra Vehicular Activity, EVA, on the Starboard, Sl, Truss of the ISS in early August 2006. The System is based on past USU SDL Space Instruments and incorporates a Floating Potential Probe, Multiple Langmuir Probes, and a Plasma Frequency Probe into one Sensor Suite. The FPMU is used to correct the Charging Models of the Station each time a New Section is added to the Structure. By providing Feedback on the Effectiveness of Steps taken to control Charging, the FPMU helps ensure a Safe Working Environment for the Astronauts.

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Details

Version:2.3.2

NumericalData

ResourceID
spase://NASA/NumericalData/ISS/FPMU/PT1S
ResourceHeader
ResourceName
ISS Floating Potential Measurement Unit (FPMU), Summary Parameter 1 s Data
ReleaseDate
2021-04-27 15:38:11Z
Description

International Space Station, ISS, Floating Potential Measurement Unit, FPMU, Ionosphere Summary Wide Langmuir Probe, WLP, Density and Narrow Langmuir Probe, NLP, Temperature Records 1 s Data. The Space Dynamics Laboratory, SDL, Utah State University, USU, developed the FPMU for the NASA Johnson Space Center. The FPMU was installed by ISS Crew Members during an Extra Vehicular Activity, EVA, on the Starboard, Sl, Truss of the ISS in early August 2006. The System is based on past USU SDL Space Instruments and incorporates a Floating Potential Probe, Multiple Langmuir Probes, and a Plasma Frequency Probe into one Sensor Suite. The FPMU is used to correct the Charging Models of the Station each time a New Section is added to the Structure. By providing Feedback on the Effectiveness of Steps taken to control Charging, the FPMU helps ensure a Safe Working Environment for the Astronauts.

Acknowledgement
R.M. Suggs, S.L. Koontz, NASA Johnson Space Center Contact Rob Suggs for support and use. Rob.Suggs@nasa.gov.
Contacts
RolePersonStartDateStopDateNote
1.PrincipalInvestigatorspase://SMWG/Person/Robert.M.Suggs
2.PrincipalInvestigatorspase://SMWG/Person/Steven.L.Koontz
3.MetadataContactspase://SMWG/Person/Robert.E.McGuire
4.MetadataContactspase://SMWG/Person/Lee.Frost.Bargatze
InformationURL
Name
Floating Potential Measurement Unit, FPMU, Home Page, SDL, USU
URL
Description

Floating Potential Measurement Unit, FPMU, Home Page, Space Dynamics Laboratory, Utah State University, per NASA Policy Directive 2200.1B, Section 1.a.5

PriorIDs
spase://VSPO/NumericalData/ISS/FPMU/PT1S
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
FTPS from SPDF (not with most browsers)
URL
Description

Access to Data in CDF Format via ftp from SPDF

AccessURL
Name
HTTPS from SPDF
URL
Description

Access to Data in CDF Format via http from SPDF

AccessURL
Name
CDAWeb
URL
ProductKey
ISS_SP_FPMU
Description

Access to ASCII, CDF, and plots via NASA/GSFC CDAWeb

Format
CDF
Encoding
None
Acknowledgement
R.M. Suggs, S.L. Koontz, NASA Johnson Space Center Contact Rob Suggs for support and use. Rob.Suggs@nasa.gov. Please acknowledge the data providers and CDAWeb when using these data.
AccessInformation
RepositoryID
Availability
Online
AccessRights
Open
AccessURL
Name
CDAWeb HAPI Server
URL
Style
HAPI
ProductKey
ISS_SP_FPMU
Description

Web Service to this product using the HAPI interface.

Format
CSV
Acknowledgement
R.M. Suggs, S.L. Koontz, NASA Johnson Space Center Contact Rob Suggs for support and use. Rob.Suggs@nasa.gov. Please acknowledge the data providers and CDAWeb when using these data.
ProcessingLevel
Calibrated
InstrumentIDs
MeasurementType
ThermalPlasma
TemporalDescription
TimeSpan
StartDate
2010-01-27 00:00:00.000
StopDate
2016-10-02 23:59:59.999
Cadence
PT1S
ObservedRegion
Earth.NearSurface.Ionosphere.FRegion
ObservedRegion
Earth.NearSurface.Thermosphere
Parameter #1
Name
Epoch Time
ParameterKey
Epoch
Description

Epoch Time, Default

Caveats
Time, dd-mm-yyyy hh:mm:ss.mms, This parameter exhibits an increasing monotonic progression.
Cadence
PT1S
Units
d
UnitsConversion
86400>s^-1
RenderingHints
AxisLabel
Epoch
ScaleType
LinearScale
ValidMin
01-Aug-2006 00:00:00.000
ValidMax
31-Dec-2059 23:59:59.999
FillValue
31-Dec-9999 23:59:59.999
Support
SupportQuantity
Temporal
Parameter #2
Name
ISS Longitude, GEO
Set
Time series defined by using: EPOCH
ParameterKey
Latitude
Description

International Space Station, ISS, Longitude, Geographic, GEO

Caveats
Geodetic Latitude
Cadence
PT1S
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GEO
RenderingHints
DisplayType
TimeSeries
AxisLabel
Latitude
ValueFormat
F7.3
ScaleType
LinearScale
ValidMin
-90.0
ValidMax
90.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #3
Name
ISS Latitude, GEO
Set
Time series defined by using: EPOCH
ParameterKey
Longitude
Description

International Space Station, ISS, Latitude, Geographic, GEO

Caveats
Geodetic Longitude
Cadence
PT1S
Units
°
UnitsConversion
0.0174532925>rad
CoordinateSystem
CoordinateRepresentation
Spherical
CoordinateSystemName
GEO
RenderingHints
DisplayType
TimeSeries
AxisLabel
Longitude
ValueFormat
F8.3
ScaleType
LinearScale
ValidMin
-180.0
ValidMax
180.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.ElevationAngle
SupportQuantity
Positional
Parameter #4
Name
ISS Altitude
Set
Time series defined by using: EPOCH
ParameterKey
Altitude
Description

International Space Station, ISS, Altitude, Geographic, GEO

Caveats
Geodetic Altitude
Cadence
PT1S
Units
km
UnitsConversion
1e3>m
RenderingHints
DisplayType
TimeSeries
AxisLabel
Altitude
ValueFormat
F8.3
ScaleType
LinearScale
ValidMin
0.0
ValidMax
500.0
FillValue
-1.0e+31
Support
Qualifier
Scalar
SupportQuantity
Other
Parameter #5
Name
Total Ion Density
Set
Time series defined by using: EPOCH
ParameterKey
N_i
Description

Total Ion Density, equal to the Electron Density

Caveats
Ion Density derived from the FPMU Wide Langmuir Probe. It can be used also for Electron Density assuming Quasi-Neutrality
Cadence
PT1S
Units
m^-3
RenderingHints
DisplayType
TimeSeries
AxisLabel
Ion Density
ValueFormat
E10.3
ValidMin
1.0e+08
ValidMax
1.0e+15
FillValue
-1.0e+31
Particle
ParticleType
Ion
Qualifier
Scalar
ParticleQuantity
NumberDensity
Parameter #6
Name
Electron Temperature
Set
Time series defined by using: EPOCH
ParameterKey
T_e
Description

Electron Temperature

Caveats
Electron temperature derived from the FPMU Narrow Langmuir Probe
Cadence
PT1S
Units
°K
RenderingHints
DisplayType
TimeSeries
AxisLabel
Electron Temperature
ValueFormat
F9.3
ScaleType
LinearScale
ValidMin
0.0
ValidMax
20000.0
FillValue
-1.0e+31
Particle
ParticleType
Electron
Qualifier
Scalar
ParticleQuantity
Temperature
Parameter #7
Name
ISS Pitch Angle
Set
Time series defined by using: EPOCH
ParameterKey
Angle
Description

International Space Station, ISS, Pitch Angle

Caveats
This ISS Pitch Attitude Information is necessary for Proper Derivation of the NLP Density. The NLP is a Cylindrical Langmuir Probe which is symmetric about the Roll and Yaw Axes.
Cadence
PT1S
Units
°
UnitsConversion
0.0174532925>rad
RenderingHints
DisplayType
TimeSeries
AxisLabel
ISS Pitch Angle
ValueFormat
F8.3
ScaleType
LinearScale
ValidMin
0.0
ValidMax
360.0
FillValue
-1.0e+31
Support
Qualifier
DirectionAngle.AzimuthAngle
SupportQuantity
Positional
Parameter #8
Name
Solar Illumination, Percent
Set
Time series defined by using: EPOCH
ParameterKey
Sunlight
Description

Solar Illumination, Percent

Caveats
Percent Solar Illumination with no Correction for Atmospheric Refraction
Cadence
PT1S
RenderingHints
DisplayType
TimeSeries
AxisLabel
Sunlight
ValueFormat
F8.3
ScaleType
LinearScale
ValidMin
0.0
ValidMax
100.0
FillValue
-1.0e+31
Support
SupportQuantity
Other
Parameter #9
Name
Time Code Correction
Set
Time series defined by using: EPOCH
ParameterKey
TCC
Description

Time Code Correction

Caveats
Flag indicating that the Time Code was Correct in Original the File, 0, or that a Corrupt Time Code was corrected during Processing, 1
Cadence
PT1S
RenderingHints
DisplayType
TimeSeries
AxisLabel
Time Code Correction
ValueFormat
I2
ScaleType
LinearScale
ValidMin
0
ValidMax
1
FillValue
-9223372036854775808
Support
SupportQuantity
InstrumentMode
Parameter #10
Name
Processing Ground Station
Set
Time series defined by using: EPOCH
ParameterKey
GS
Description

Processing Ground Station

Caveats
Processing Ground Station could be JSC, MSFC, or HSV.
Cadence
PT1S
RenderingHints
AxisLabel
ground_station
ValueFormat
A5
Support
SupportQuantity
Other