diff --git a/Instrument/AMDA/Cluster-Tango/EFW.xml b/Instrument/AMDA/Cluster-Tango/EFW.xml index 86c586d..e429ad4 100644 --- a/Instrument/AMDA/Cluster-Tango/EFW.xml +++ b/Instrument/AMDA/Cluster-Tango/EFW.xml @@ -4,8 +4,8 @@ spase://CDPP/Instrument/AMDA/Cluster-Tango/EFW - Electric Field and Waves (EFW) - EFW + EFW + Electric Field and Waves 2011-02-04T15:37:19Z The EFW (Electric Field and Waves) instrument consists of four orthogonal spherical sensors deployed from 50 m cable booms in the spin plane of the spacecraft, plus four deployment units and a main electronics unit. Each deployment unit deploys a multiconductor cable and tip-mounted spherical sensor. Each opposing pair of cables will be symmetrically deployed to a tip-to-tip distance of approximately 100 m, except for about a week at the beginning of the mission when 70 m will be used for one boom pair (the Z-booms) and 100 m for the other pair. The potentials of the spherical sensor and nearby conductors are controlled by the microprocessor to minimize errors associated with photoelectron fluxes to and from the spheres. Output signals from the sensor preamplifiers are provided to the wave instruments for analysis of high frequency wave phenomena. There is a 1 MB burst memory and tow fast A/D conversion circuits for recording electric field wave forms for time resolutions of up to 36,000 samples/s. Data gathered in the burst memory will be played back through the telemetry stream allocated to the instrument by pre-empting a portion of the real-time data. Incoming data are continuously monitored by algorithms in the software to determine whether to trigger the burst-playback mode. A large number of sampling modes is possible, yielding four possible telemetry rates from 1.440--29.440 Kbps. This data stream is transferred via the DWP instrument. The main measured quantities will be, in various modes: (1) the instantaneous spin-plane components of the electric field vector, from 0.1--700 V/Km, with time resolution down to 0.1 ms, in four frequency ranges from DC to upper limits of 10 Hz, 180 Hz, 4 KHz, or 32 KHz; (2) the AC electric field components from 10 Hz to 8 KHz, within the dynamic range of ~3 mV/Km to 10 V/Km; (3) plasma density fluctuations within the range of 1--100/cm and in three frequency ranges from 0 Hz to upper limits of 10 Hz, 180 Hz, or 4 KHz; and, (4) density and temperature (in Langmuir sweeps) in the eV range, with a dynamic range of 1--100/cm. There is also a frequency counter covering the range 10--200 KHz. On-board calculations of least-square fits to the electric field data over one spacecraft spin period (4 s) will provide a baseline of high-quality two-dimensional electric field components that are present in the telemetry stream, except for periods when three or four sensors are in current mode. The spacecraft potential is calculated and transmitted via DWP to other instruments on board. The three components from the search coil instrument (WHISPER) are also available in EFW with a bandwidth of 4 KHz. For more details of the Cluster mission, the spacecraft, and its instruments, see the report ``Cluster: mission, payload and supporting activities,'' March 1993, ESA SP-1159, and the included article ``The Spherical Probe Electric Field and Wave Experiment for the Cluster Mission,'' by G. Gustafsson et al., from which this information was obtained. diff --git a/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-efw-gse.xml b/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-efw-gse.xml index 701d822..c037a96 100644 --- a/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-efw-gse.xml +++ b/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-efw-gse.xml @@ -4,11 +4,16 @@ spase://CDPP/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-efw-gse - efield gse + 3d (gse) Cluster 1 Prime Parameter EFW Data 2015-10-19T11:00:44Z - The EFW (Electric Field and Waves) instrument consists of four orthogonal spherical sensors deployed from 50 m cable booms in the spin plane of the spacecraft, plus four deployment units and a main electronics unit. Each deployment unit deploys a multiconductor cable and tip-mounted spherical sensor. Each opposing pair of cables will be symmetrically deployed to a tip-to-tip distance of approximately 100 m, except for about a week at the beginning of the mission when 70 m will be used for one boom pair (the Z-booms) and 100 m for the other pair. The potentials of the spherical sensor and nearby conductors are controlled by the microprocessor to minimize errors associated with photoelectron fluxes to and from the spheres. Output signals from the sensor preamplifiers are provided to the wave instruments for analysis of high frequency wave phenomena. There is a 1 MB burst memory and tow fast A/D conversion circuits for recording electric field wave forms for time resolutions of up to 36,000 samples/s. Data gathered in the burst memory will be played back through the telemetry stream allocated to the instrument by pre-empting a portion of the real-time data. Incoming data are continuously monitored by algorithms in the software to determine whether to trigger the burst-playback mode. A large number of sampling modes is possible, yielding four possible telemetry rates from 1.440-29.440 Kbps. This data stream is transferred via the DWP instrument. The main measured quantities will be, in various modes: (1) the instantaneous spin-plane components of the electric field vector, from 0.1-700 V/Km, with time resolution down to 0.1 ms, in four frequency ranges from DC to upper limits of 10 Hz, 180 Hz, 4 KHz, or 32 KHz; (2) the AC electric field components from 10 Hz to 8 KHz, within the dynamic range of ~3 mV/Km to 10 V/Km; (3) plasma density fluctuations within the range of 1-100/cm and in three frequency ranges from 0 Hz to upper limits of 10 Hz, 180 Hz, or 4 KHz; and, (4) density and temperature (in Langmuir sweeps) in the eV range, with a dynamic range of 1-100/cm. There is also a frequency counter covering the range 10-200 KHz. On-board calculations of least-square fits to the electric field data over one spacecraft spin period (4 s) will provide a baseline of high-quality two-dimensional electric field components that are present in the telemetry stream, except for periods when three or four sensors are in current mode. The spacecraft potential is calculated and transmitted via DWP to other instruments on board. The three components from the search coil instrument (WHISPER) are also available in EFW with a bandwidth of 4 KHz. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The Spherical Probe Electric Field and Waves experiment for the Cluster Mission, by G. Gustafsson et al., from which this information was obtained. - NASA, Georg Gustafsson + + Electric Field in GSE is obtained from CSA C[1-4]_CP_EFW_L3_E3D_GSE + Note that Pi has not validated this product. + This dataset contains the electric field in the inertial frame (i.e., vxB removed) in the GSE coordinate system, using EFW electric field data from file C[1-4]_CP_EFW_L3_E and interpolated FGM magnetic field data from C[1-4]_CP_FGM_5VPS products. The spin-axis component of the electric field is calculated with assumption of E.B equals 0 and with use of 2 electric field + components in the spin plane and three magnetic field components. + + NASA, Georg Gustafsson spase://SMWG/Person/Elena.Budnik TechnicalContact @@ -17,7 +22,12 @@ NSSDC Master Catalog listing for Cluster II Rumba Electric Field and Waves (EFW) http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=2000-045A-08 This site provides information concerning the Cluster II Rumba Electric Field and Waves Instrument. - + + + c1-efw-efield + PartOf + electric field + spase://SMWG/Repository/CDPP/AMDA @@ -67,7 +77,7 @@ magnetotail lobe - Duskward Electric Field Vector + e_gse c1_e_gse Cluster II Rumba Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -84,28 +94,29 @@ 3 - ex_gse + ex 1 c1_e_gse(0) - ey_gse + ey 2 c1_e_gse(1) - ez_gse + ez 3 c1_e_gse(2) + -1.e31 Vector Electric - Duskward Electric Field Vector + e_gsm c1_e_gsm Cluster II Rumba Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -122,17 +133,17 @@ 3 - ex_gsm + ex 1 c1_e_gsm(0) - ey_gsm + ey 2 c1_e_gsm(1) - ez_gsm + ez 3 c1_e_gsm(2) @@ -143,7 +154,7 @@ - Electric Field Magnitude + |e| c1_etot Cluster II Rumba Prime Parameter Electric Field Magnitude at spin time resolution phys.elecField @@ -153,13 +164,14 @@ TimeSeries + -1.e31 Scalar Electric - e_gse_quality + e_quality c1_e_gse_qual meta.code.qual PT4S @@ -171,13 +183,14 @@ - ez_gse_error + ez_error c1_ez_error stat.error PT4S TimeSeries + -1.e31 Other diff --git a/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-efw-sr2.xml b/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-efw-sr2.xml index c6f9f8f..f549c03 100644 --- a/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-efw-sr2.xml +++ b/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-efw-sr2.xml @@ -4,10 +4,15 @@ spase://CDPP/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-efw-sr2 - efield sr2 + isr2 Cluster 1 Prime Parameter EFW Data 2015-10-16T15:51:44Z - The EFW (Electric Field and Waves) instrument consists of four orthogonal spherical sensors deployed from 50 m cable booms in the spin plane of the spacecraft, plus four deployment units and a main electronics unit. Each deployment unit deploys a multiconductor cable and tip-mounted spherical sensor. Each opposing pair of cables will be symmetrically deployed to a tip-to-tip distance of approximately 100 m, except for about a week at the beginning of the mission when 70 m will be used for one boom pair (the Z-booms) and 100 m for the other pair. The potentials of the spherical sensor and nearby conductors are controlled by the microprocessor to minimize errors associated with photoelectron fluxes to and from the spheres. Output signals from the sensor preamplifiers are provided to the wave instruments for analysis of high frequency wave phenomena. There is a 1 MB burst memory and tow fast A/D conversion circuits for recording electric field wave forms for time resolutions of up to 36,000 samples/s. Data gathered in the burst memory will be played back through the telemetry stream allocated to the instrument by pre-empting a portion of the real-time data. Incoming data are continuously monitored by algorithms in the software to determine whether to trigger the burst-playback mode. A large number of sampling modes is possible, yielding four possible telemetry rates from 1.440-29.440 Kbps. This data stream is transferred via the DWP instrument. The main measured quantities will be, in various modes: (1) the instantaneous spin-plane components of the electric field vector, from 0.1-700 V/Km, with time resolution down to 0.1 ms, in four frequency ranges from DC to upper limits of 10 Hz, 180 Hz, 4 KHz, or 32 KHz; (2) the AC electric field components from 10 Hz to 8 KHz, within the dynamic range of ~3 mV/Km to 10 V/Km; (3) plasma density fluctuations within the range of 1-100/cm and in three frequency ranges from 0 Hz to upper limits of 10 Hz, 180 Hz, or 4 KHz; and, (4) density and temperature (in Langmuir sweeps) in the eV range, with a dynamic range of 1-100/cm. There is also a frequency counter covering the range 10-200 KHz. On-board calculations of least-square fits to the electric field data over one spacecraft spin period (4 s) will provide a baseline of high-quality two-dimensional electric field components that are present in the telemetry stream, except for periods when three or four sensors are in current mode. The spacecraft potential is calculated and transmitted via DWP to other instruments on board. The three components from the search coil instrument (WHISPER) are also available in EFW with a bandwidth of 4 KHz. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The Spherical Probe Electric Field and Waves experiment for the Cluster Mission, by G. Gustafsson et al., from which this information was obtained. + Electric Field in ISR2 is obtained from CAA C[1-4]_CP_EFW_L3_E + + The EFW instrument measures the electric field only in the spacecraft + spin plane, therefore a spin-plane oriented coordinate system is best suited for scientific studies involving the electric field. The ISR2 (Inverted Spin Reference) system, also known as DSI (Despun System Inverted), is such a system. The X and Y axes are in the spin plane, with X pointing as near sunward as possible and Y perpendicular to the sunward direction, positive towards dusk. The Z-axis is along the (negative) spacecraft spin axis, towards the north ecliptic. The coordinate system is called Inverted because the actual spin axis of Cluster is pointing towards the south ecliptic. The difference between ISR2 (DSI) and the GSE (Geocentric Solar Ecliptic) is a tilt of 2° to 7° of the Z-axis performed in order + to avoid shading of the EFW probes by the spacecraft. + NASA, Georg Gustafsson spase://SMWG/Person/Elena.Budnik @@ -17,7 +22,12 @@ NSSDC Master Catalog listing for Cluster II Rumba Electric Field and Waves (EFW) http://nssdc.gsfc.nasa.gov/nmc/experimentDisplay.do?id=2000-045A-08 This site provides information concerning the Cluster II Rumba Electric Field and Waves Instrument. - + + + c1-efw-efield + PartOf + electric field + spase://SMWG/Repository/CDPP/AMDA @@ -67,7 +77,7 @@ magnetotail lobe - Duskward Electric Field Vector + e_sr2 c1_e_sr2 Cluster II Rumba Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -76,7 +86,7 @@ 1.0e-3>V m^-1 Cartesian - GSE + SR2 TimeSeries @@ -89,18 +99,19 @@ c1_e_sr2(0) - ex + ey 2 c1_e_sr2(1) + -1.e9 Vector Electric - e_sr2_quality + e_quality c1_e_sr2_qual meta.code.qual PT4S diff --git a/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-pot-full.xml b/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-pot-full.xml index 1413ccc..848bd70 100644 --- a/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-pot-full.xml +++ b/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-pot-full.xml @@ -21,7 +21,7 @@ c1-efw-pot PartOf - probe potential + s/c potential diff --git a/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-pot-spin.xml b/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-pot-spin.xml index bf0d656..582ac2f 100644 --- a/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-pot-spin.xml +++ b/NumericalData/AMDA/Cluster/Cluster1/EFW/clust1-pot-spin.xml @@ -21,7 +21,7 @@ c1-efw-pot PartOf - probe potential + s/c potential diff --git a/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-efw-gse.xml b/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-efw-gse.xml index e2ed94f..574c77b 100644 --- a/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-efw-gse.xml +++ b/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-efw-gse.xml @@ -4,10 +4,14 @@ spase://CDPP/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-efw-gse - Cluster II Salsa Prime Parameter Electric Field and Waves (EFW) Data + 3d (gse) Cluster 2 Prime Parameter EFW Data 2015-10-19T15:51:44Z - The EFW (Electric Field and Waves) instrument consists of four orthogonal spherical sensors deployed from 50 m cable booms in the spin plane of the spacecraft, plus four deployment units and a main electronics unit. Each deployment unit deploys a multiconductor cable and tip-mounted spherical sensor. Each opposing pair of cables will be symmetrically deployed to a tip-to-tip distance of approximately 100 m, except for about a week at the beginning of the mission when 70 m will be used for one boom pair (the Z-booms) and 100 m for the other pair. The potentials of the spherical sensor and nearby conductors are controlled by the microprocessor to minimize errors associated with photoelectron fluxes to and from the spheres. Output signals from the sensor preamplifiers are provided to the wave instruments for analysis of high frequency wave phenomena. There is a 1 MB burst memory and tow fast A/D conversion circuits for recording electric field wave forms for time resolutions of up to 36,000 samples/s. Data gathered in the burst memory will be played back through the telemetry stream allocated to the instrument by pre-empting a portion of the real-time data. Incoming data are continuously monitored by algorithms in the software to determine whether to trigger the burst-playback mode. A large number of sampling modes is possible, yielding four possible telemetry rates from 1.440-29.440 Kbps. This data stream is transferred via the DWP instrument. The main measured quantities will be, in various modes: (1) the instantaneous spin-plane components of the electric field vector, from 0.1-700 V/Km, with time resolution down to 0.1 ms, in four frequency ranges from DC to upper limits of 10 Hz, 180 Hz, 4 KHz, or 32 KHz; (2) the AC electric field components from 10 Hz to 8 KHz, within the dynamic range of ~3 mV/Km to 10 V/Km; (3) plasma density fluctuations within the range of 1-100/cm and in three frequency ranges from 0 Hz to upper limits of 10 Hz, 180 Hz, or 4 KHz; and, (4) density and temperature (in Langmuir sweeps) in the eV range, with a dynamic range of 1-100/cm. There is also a frequency counter covering the range 10-200 KHz. On-board calculations of least-square fits to the electric field data over one spacecraft spin period (4 s) will provide a baseline of high-quality two-dimensional electric field components that are present in the telemetry stream, except for periods when three or four sensors are in current mode. The spacecraft potential is calculated and transmitted via DWP to other instruments on board. The three components from the search coil instrument (WHISPER) are also available in EFW with a bandwidth of 4 KHz. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The Spherical Probe Electric Field and Waves experiment for the Cluster Mission, by G. Gustafsson et al., from which this information was obtained. + Electric Field in GSE is obtained from CSA C[1-4]_CP_EFW_L3_E3D_GSE + Note that Pi has not validated this product. + This dataset contains the electric field in the inertial frame (i.e., vxB removed) in the GSE coordinate system, using EFW electric field data from file C[1-4]_CP_EFW_L3_E and interpolated FGM magnetic field data from C[1-4]_CP_FGM_5VPS products. The spin-axis component of the electric field is calculated with assumption of E.B equals 0 and with use of 2 electric field + components in the spin plane and three magnetic field components. + NASA, Georg Gustafsson spase://SMWG/Person/Elena.Budnik @@ -19,8 +23,9 @@ This site provides information concerning the Cluster II Salsa Electric Field and Waves Instrument. - spase://SMWG/Observatory/Cluster-Salsa - ObservedBy + c2-efw-efield + PartOf + electric field @@ -71,7 +76,7 @@ magnetotail lobe - Duskward Electric Field Vector + e_gse c2_e_gse Cluster II Salsa Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -88,28 +93,29 @@ 3 - ex_gse + ex 1 c2_e_gse(0) - ey_gse + ey 2 c2_e_gse(1) - ez_gse + ez 3 c2_e_gse(2) + -1.e31 Vector Electric - Duskward Electric Field Vector + e_gsm c2_e_gsm Cluster II Salsa Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -126,17 +132,17 @@ 3 - ex_gsm + ex 1 c2_e_gsm(0) - ey_gsm + ey 2 c2_e_gsm(1) - ez_gsm + ez 3 c2_e_gsm(2) @@ -147,7 +153,7 @@ - Electric Field Magnitude + |e| c2_etot Cluster II Salsa Prime Parameter Electric Field Magnitude at spin time resolution phys.elecField @@ -157,13 +163,14 @@ TimeSeries + -1.e31 Scalar Electric - e_gse_quality + e_quality c2_e_gse_qual PT4S @@ -171,13 +178,14 @@ - ez_gse_error + ez_error c2_ez_error stat.error PT4S TimeSeries + -1.e31 Other diff --git a/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-efw-sr2.xml b/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-efw-sr2.xml index d99df77..6ab6263 100644 --- a/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-efw-sr2.xml +++ b/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-efw-sr2.xml @@ -4,10 +4,14 @@ spase://CDPP/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-efw-sr2 - Cluster II Rumba Prime Parameter Electric Field and Waves (EFW) Data + isr2 Cluster 1 Prime Parameter EFW Data 2015-10-19T15:51:44Z - The EFW (Electric Field and Waves) instrument consists of four orthogonal spherical sensors deployed from 50 m cable booms in the spin plane of the spacecraft, plus four deployment units and a main electronics unit. Each deployment unit deploys a multiconductor cable and tip-mounted spherical sensor. Each opposing pair of cables will be symmetrically deployed to a tip-to-tip distance of approximately 100 m, except for about a week at the beginning of the mission when 70 m will be used for one boom pair (the Z-booms) and 100 m for the other pair. The potentials of the spherical sensor and nearby conductors are controlled by the microprocessor to minimize errors associated with photoelectron fluxes to and from the spheres. Output signals from the sensor preamplifiers are provided to the wave instruments for analysis of high frequency wave phenomena. There is a 1 MB burst memory and tow fast A/D conversion circuits for recording electric field wave forms for time resolutions of up to 36,000 samples/s. Data gathered in the burst memory will be played back through the telemetry stream allocated to the instrument by pre-empting a portion of the real-time data. Incoming data are continuously monitored by algorithms in the software to determine whether to trigger the burst-playback mode. A large number of sampling modes is possible, yielding four possible telemetry rates from 1.440-29.440 Kbps. This data stream is transferred via the DWP instrument. The main measured quantities will be, in various modes: (1) the instantaneous spin-plane components of the electric field vector, from 0.1-700 V/Km, with time resolution down to 0.1 ms, in four frequency ranges from DC to upper limits of 10 Hz, 180 Hz, 4 KHz, or 32 KHz; (2) the AC electric field components from 10 Hz to 8 KHz, within the dynamic range of ~3 mV/Km to 10 V/Km; (3) plasma density fluctuations within the range of 1-100/cm and in three frequency ranges from 0 Hz to upper limits of 10 Hz, 180 Hz, or 4 KHz; and, (4) density and temperature (in Langmuir sweeps) in the eV range, with a dynamic range of 1-100/cm. There is also a frequency counter covering the range 10-200 KHz. On-board calculations of least-square fits to the electric field data over one spacecraft spin period (4 s) will provide a baseline of high-quality two-dimensional electric field components that are present in the telemetry stream, except for periods when three or four sensors are in current mode. The spacecraft potential is calculated and transmitted via DWP to other instruments on board. The three components from the search coil instrument (WHISPER) are also available in EFW with a bandwidth of 4 KHz. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The Spherical Probe Electric Field and Waves experiment for the Cluster Mission, by G. Gustafsson et al., from which this information was obtained. + Electric Field in ISR2 is obtained from CAA C[1-4]_CP_EFW_L3_E + + The EFW instrument measures the electric field only in the spacecraft + spin plane, therefore a spin-plane oriented coordinate system is best suited for scientific studies involving the electric field. The ISR2 (Inverted Spin Reference) system, also known as DSI (Despun System Inverted), is such a system. The X and Y axes are in the spin plane, with X pointing as near sunward as possible and Y perpendicular to the sunward direction, positive towards dusk. The Z-axis is along the (negative) spacecraft spin axis, towards the north ecliptic. The coordinate system is called Inverted because the actual spin axis of Cluster is pointing towards the south ecliptic. The difference between ISR2 (DSI) and the GSE (Geocentric Solar Ecliptic) is a tilt of 2° to 7° of the Z-axis performed in order + to avoid shading of the EFW probes by the spacecraft. NASA, Georg Gustafsson spase://SMWG/Person/Elena.Budnik @@ -19,8 +23,9 @@ This site provides information concerning the Cluster II Salsa Electric Field and Waves Instrument. - spase://SMWG/Observatory/Cluster-Salsa - ObservedBy + c2-efw-efield + PartOf + electric field @@ -71,7 +76,7 @@ magnetotail lobe - Duskward Electric Field Vector + e_sr2 c2_e_sr2 Cluster II Salsa Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -80,7 +85,7 @@ 1.0e-3>V m^-1 Cartesian - GSE + SR2 TimeSeries @@ -93,18 +98,19 @@ c2_e_sr2(0) - ex + ey 2 c2_e_sr2(1) + -1.e9 Vector Electric - e_sr2_quality + e_quality c2_e_sr2_qual meta.code.qual PT4S diff --git a/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-pot-full.xml b/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-pot-full.xml index 95a9f97..9aaaa16 100644 --- a/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-pot-full.xml +++ b/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-pot-full.xml @@ -21,7 +21,7 @@ c2-efw-pot PartOf - probe potential + s/c potential diff --git a/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-pot-spin.xml b/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-pot-spin.xml index 4711b78..3a9acc0 100644 --- a/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-pot-spin.xml +++ b/NumericalData/AMDA/Cluster/Cluster2/EFW/clust2-pot-spin.xml @@ -21,7 +21,7 @@ c2-efw-pot PartOf - probe potential + s/c potential diff --git a/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-efw-gse.xml b/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-efw-gse.xml index d45db27..74a92e1 100644 --- a/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-efw-gse.xml +++ b/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-efw-gse.xml @@ -4,11 +4,15 @@ spase://CDPP/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-efw-gse - Cluster II Samba Prime Parameter Electric Field and Waves (EFW) Data + 3d (gse) Cluster 3 Prime Parameter EFW Data 2015-10-19T15:51:44Z - The EFW (Electric Field and Waves) instrument consists of four orthogonal spherical sensors deployed from 50 m cable booms in the spin plane of the spacecraft, plus four deployment units and a main electronics unit. Each deployment unit deploys a multiconductor cable and tip-mounted spherical sensor. Each opposing pair of cables will be symmetrically deployed to a tip-to-tip distance of approximately 100 m, except for about a week at the beginning of the mission when 70 m will be used for one boom pair (the Z-booms) and 100 m for the other pair. The potentials of the spherical sensor and nearby conductors are controlled by the microprocessor to minimize errors associated with photoelectron fluxes to and from the spheres. Output signals from the sensor preamplifiers are provided to the wave instruments for analysis of high frequency wave phenomena. There is a 1 MB burst memory and tow fast A/D conversion circuits for recording electric field wave forms for time resolutions of up to 36,000 samples/s. Data gathered in the burst memory will be played back through the telemetry stream allocated to the instrument by pre-empting a portion of the real-time data. Incoming data are continuously monitored by algorithms in the software to determine whether to trigger the burst-playback mode. A large number of sampling modes is possible, yielding four possible telemetry rates from 1.440-29.440 Kbps. This data stream is transferred via the DWP instrument. The main measured quantities will be, in various modes: (1) the instantaneous spin-plane components of the electric field vector, from 0.1-700 V/Km, with time resolution down to 0.1 ms, in four frequency ranges from DC to upper limits of 10 Hz, 180 Hz, 4 KHz, or 32 KHz; (2) the AC electric field components from 10 Hz to 8 KHz, within the dynamic range of ~3 mV/Km to 10 V/Km; (3) plasma density fluctuations within the range of 1-100/cm and in three frequency ranges from 0 Hz to upper limits of 10 Hz, 180 Hz, or 4 KHz; and, (4) density and temperature (in Langmuir sweeps) in the eV range, with a dynamic range of 1-100/cm. There is also a frequency counter covering the range 10-200 KHz. On-board calculations of least-square fits to the electric field data over one spacecraft spin period (4 s) will provide a baseline of high-quality two-dimensional electric field components that are present in the telemetry stream, except for periods when three or four sensors are in current mode. The spacecraft potential is calculated and transmitted via DWP to other instruments on board. The three components from the search coil instrument (WHISPER) are also available in EFW with a bandwidth of 4 KHz. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The Spherical Probe Electric Field and Waves experiment for the Cluster Mission, by G. Gustafsson et al., from which this information was obtained. - NASA, Georg Gustafsson + Electric Field in GSE is obtained from CSA C[1-4]_CP_EFW_L3_E3D_GSE + Note that Pi has not validated this product. + This dataset contains the electric field in the inertial frame (i.e., vxB removed) in the GSE coordinate system, using EFW electric field data from file C[1-4]_CP_EFW_L3_E and interpolated FGM magnetic field data from C[1-4]_CP_FGM_5VPS products. The spin-axis component of the electric field is calculated with assumption of E.B equals 0 and with use of 2 electric field + components in the spin plane and three magnetic field components. + + NASA, Georg Gustafsson spase://SMWG/Person/Elena.Budnik TechnicalContact @@ -19,8 +23,9 @@ This site provides information concerning the Cluster II Samba Electric Field and Waves Instrument. - spase://SMWG/Observatory/Cluster-Samba - ObservedBy + c3-efw-efield + PartOf + electric field @@ -71,7 +76,7 @@ magnetotail lobe - Duskward Electric Field Vector + e_gse c3_e_gse Cluster II Samba Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -88,28 +93,29 @@ 3 - ex_gse + ex 1 c3_e_gse(0) - ey_gse + ey 2 c3_e_gse(1) - ez_gse + ez 3 c3_e_gse(2) + -1.e31 Vector Electric - Duskward Electric Field Vector + e_gsm c3_e_gsm Cluster II Samba Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -126,17 +132,17 @@ 3 - ex_gsm + ex 1 c3_e_gsm(0) - ey_gsm + ey 2 c3_e_gsm(1) - ez_gsm + ez 3 c3_e_gsm(2) @@ -147,7 +153,7 @@ - Electric Field Magnitude + |e| c3_etot Cluster II Samba Prime Parameter Electric Field Magnitude at spin time resolution phys.elecField @@ -157,13 +163,14 @@ TimeSeries + -1.e31 Scalar Electric - e_gse_quality + e_quality c3_e_gse_qual meta.code.qual PT4S @@ -175,13 +182,14 @@ - ez_gse_error + ez_error c3_ez_error stat.error PT4S TimeSeries + -1.e31 Other diff --git a/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-efw-sr2.xml b/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-efw-sr2.xml index 986555d..8b4348f 100644 --- a/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-efw-sr2.xml +++ b/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-efw-sr2.xml @@ -4,10 +4,14 @@ spase://CDPP/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-efw-sr2 - Cluster II Samba Prime Parameter Electric Field and Waves (EFW) Data + isr2 Cluster 3 Prime Parameter EFW Data 2015-10-19T15:51:44Z - The EFW (Electric Field and Waves) instrument consists of four orthogonal spherical sensors deployed from 50 m cable booms in the spin plane of the spacecraft, plus four deployment units and a main electronics unit. Each deployment unit deploys a multiconductor cable and tip-mounted spherical sensor. Each opposing pair of cables will be symmetrically deployed to a tip-to-tip distance of approximately 100 m, except for about a week at the beginning of the mission when 70 m will be used for one boom pair (the Z-booms) and 100 m for the other pair. The potentials of the spherical sensor and nearby conductors are controlled by the microprocessor to minimize errors associated with photoelectron fluxes to and from the spheres. Output signals from the sensor preamplifiers are provided to the wave instruments for analysis of high frequency wave phenomena. There is a 1 MB burst memory and tow fast A/D conversion circuits for recording electric field wave forms for time resolutions of up to 36,000 samples/s. Data gathered in the burst memory will be played back through the telemetry stream allocated to the instrument by pre-empting a portion of the real-time data. Incoming data are continuously monitored by algorithms in the software to determine whether to trigger the burst-playback mode. A large number of sampling modes is possible, yielding four possible telemetry rates from 1.440-29.440 Kbps. This data stream is transferred via the DWP instrument. The main measured quantities will be, in various modes: (1) the instantaneous spin-plane components of the electric field vector, from 0.1-700 V/Km, with time resolution down to 0.1 ms, in four frequency ranges from DC to upper limits of 10 Hz, 180 Hz, 4 KHz, or 32 KHz; (2) the AC electric field components from 10 Hz to 8 KHz, within the dynamic range of ~3 mV/Km to 10 V/Km; (3) plasma density fluctuations within the range of 1-100/cm and in three frequency ranges from 0 Hz to upper limits of 10 Hz, 180 Hz, or 4 KHz; and, (4) density and temperature (in Langmuir sweeps) in the eV range, with a dynamic range of 1-100/cm. There is also a frequency counter covering the range 10-200 KHz. On-board calculations of least-square fits to the electric field data over one spacecraft spin period (4 s) will provide a baseline of high-quality two-dimensional electric field components that are present in the telemetry stream, except for periods when three or four sensors are in current mode. The spacecraft potential is calculated and transmitted via DWP to other instruments on board. The three components from the search coil instrument (WHISPER) are also available in EFW with a bandwidth of 4 KHz. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The Spherical Probe Electric Field and Waves experiment for the Cluster Mission, by G. Gustafsson et al., from which this information was obtained. + Electric Field in ISR2 is obtained from CAA C[1-4]_CP_EFW_L3_E + + The EFW instrument measures the electric field only in the spacecraft + spin plane, therefore a spin-plane oriented coordinate system is best suited for scientific studies involving the electric field. The ISR2 (Inverted Spin Reference) system, also known as DSI (Despun System Inverted), is such a system. The X and Y axes are in the spin plane, with X pointing as near sunward as possible and Y perpendicular to the sunward direction, positive towards dusk. The Z-axis is along the (negative) spacecraft spin axis, towards the north ecliptic. The coordinate system is called Inverted because the actual spin axis of Cluster is pointing towards the south ecliptic. The difference between ISR2 (DSI) and the GSE (Geocentric Solar Ecliptic) is a tilt of 2° to 7° of the Z-axis performed in order + to avoid shading of the EFW probes by the spacecraft. NASA, Georg Gustafsson spase://SMWG/Person/Elena.Budnik @@ -19,8 +23,9 @@ This site provides information concerning the Cluster II Samba Electric Field and Waves Instrument. - spase://SMWG/Observatory/Cluster-Samba - ObservedBy + c3-efw-efield + PartOf + electric field @@ -71,7 +76,7 @@ magnetotail lobe - Duskward Electric Field Vector + e_sr2 c3_e_sr2 Cluster II Samba Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -80,7 +85,7 @@ 1.0e-3>V m^-1 Cartesian - GSE + SR2 TimeSeries @@ -93,11 +98,12 @@ c3_e_sr2(0) - ex + ey 2 c3_e_sr2(1) + -1.e9 Vector Electric diff --git a/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-pot-full.xml b/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-pot-full.xml index 9cfbd77..7beb3b2 100644 --- a/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-pot-full.xml +++ b/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-pot-full.xml @@ -21,7 +21,7 @@ c3-efw-pot PartOf - probe potential + s/c potential diff --git a/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-pot-spin.xml b/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-pot-spin.xml index f3880f6..4feb734 100644 --- a/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-pot-spin.xml +++ b/NumericalData/AMDA/Cluster/Cluster3/EFW/clust3-pot-spin.xml @@ -21,7 +21,7 @@ c3-efw-pot PartOf - probe potential + s/c potential diff --git a/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-efw-gse.xml b/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-efw-gse.xml index 655531c..e2b0316 100644 --- a/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-efw-gse.xml +++ b/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-efw-gse.xml @@ -4,10 +4,14 @@ spase://CDPP/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-efw-gse - Cluster II Tango Prime Parameter Electric Field and Waves (EFW) Data + 3d (gse) Cluster 4 Prime Parameter EFW Data 2014-12-08T15:51:44Z - The EFW (Electric Field and Waves) instrument consists of four orthogonal spherical sensors deployed from 50 m cable booms in the spin plane of the spacecraft, plus four deployment units and a main electronics unit. Each deployment unit deploys a multiconductor cable and tip-mounted spherical sensor. Each opposing pair of cables will be symmetrically deployed to a tip-to-tip distance of approximately 100 m, except for about a week at the beginning of the mission when 70 m will be used for one boom pair (the Z-booms) and 100 m for the other pair. The potentials of the spherical sensor and nearby conductors are controlled by the microprocessor to minimize errors associated with photoelectron fluxes to and from the spheres. Output signals from the sensor preamplifiers are provided to the wave instruments for analysis of high frequency wave phenomena. There is a 1 MB burst memory and tow fast A/D conversion circuits for recording electric field wave forms for time resolutions of up to 36,000 samples/s. Data gathered in the burst memory will be played back through the telemetry stream allocated to the instrument by pre-empting a portion of the real-time data. Incoming data are continuously monitored by algorithms in the software to determine whether to trigger the burst-playback mode. A large number of sampling modes is possible, yielding four possible telemetry rates from 1.440-29.440 Kbps. This data stream is transferred via the DWP instrument. The main measured quantities will be, in various modes: (1) the instantaneous spin-plane components of the electric field vector, from 0.1-700 V/Km, with time resolution down to 0.1 ms, in four frequency ranges from DC to upper limits of 10 Hz, 180 Hz, 4 KHz, or 32 KHz; (2) the AC electric field components from 10 Hz to 8 KHz, within the dynamic range of ~3 mV/Km to 10 V/Km; (3) plasma density fluctuations within the range of 1-100/cm and in three frequency ranges from 0 Hz to upper limits of 10 Hz, 180 Hz, or 4 KHz; and, (4) density and temperature (in Langmuir sweeps) in the eV range, with a dynamic range of 1-100/cm. There is also a frequency counter covering the range 10-200 KHz. On-board calculations of least-square fits to the electric field data over one spacecraft spin period (4 s) will provide a baseline of high-quality two-dimensional electric field components that are present in the telemetry stream, except for periods when three or four sensors are in current mode. The spacecraft potential is calculated and transmitted via DWP to other instruments on board. The three components from the search coil instrument (WHISPER) are also available in EFW with a bandwidth of 4 KHz. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The Spherical Probe Electric Field and Waves experiment for the Cluster Mission, by G. Gustafsson et al., from which this information was obtained. + Electric Field in GSE is obtained from CSA C[1-4]_CP_EFW_L3_E3D_GSE + Note that Pi has not validated this product. + This dataset contains the electric field in the inertial frame (i.e., vxB removed) in the GSE coordinate system, using EFW electric field data from file C[1-4]_CP_EFW_L3_E and interpolated FGM magnetic field data from C[1-4]_CP_FGM_5VPS products. The spin-axis component of the electric field is calculated with assumption of E.B equals 0 and with use of 2 electric field + components in the spin plane and three magnetic field components. + NASA, Georg Gustafsson spase://SMWG/Person/Elena.Budnik @@ -19,8 +23,9 @@ This site provides information concerning the Cluster II Tango Electric Field and Waves Instrument. - spase://SMWG/Observatory/Cluster-Tango - ObservedBy + c4-efw-efield + PartOf + electric field @@ -71,7 +76,7 @@ magnetotail lobe - Duskward Electric Field Vector + e-gse c4_e_gse Cluster II Tango Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -88,28 +93,29 @@ 3 - ex_gse + ex 1 c4_e_gse(0) - ey_gse + ey 2 c4_e_gse(1) - ez_gse + ez 3 c4_e_gse(2) + -1.e31 Vector Electric - Duskward Electric Field Vector + e_gsm c4_e_gsm Cluster II Tango Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -126,17 +132,17 @@ 3 - ex_gsm + ex 1 c4_e_gsm(0) - ey_gsm + ey 2 c4_e_gsm(1) - ez_gsm + ez 3 c4_e_gsm(2) @@ -147,7 +153,7 @@ - Electric Field Magnitude + |e| c4_etot Cluster II Tango Prime Parameter Electric Field Magnitude at spin time resolution phys.elecField @@ -157,13 +163,14 @@ TimeSeries + -1.e31 Scalar Electric - e_gse_quality + e_quality c4_e_gse_qual meta.code.qual PT4S @@ -175,13 +182,14 @@ - ez_gse_error + ez_error c4_ez_error stat.error PT4S TimeSeries + -1.e31 Other diff --git a/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-efw-sr2.xml b/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-efw-sr2.xml index 6db0d1d..817b940 100644 --- a/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-efw-sr2.xml +++ b/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-efw-sr2.xml @@ -4,10 +4,14 @@ spase://CDPP/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-efw-sr2 - Cluster II Tango Prime Parameter Electric Field and Waves (EFW) Data + isr2 Cluster 4 Prime Parameter EFW Data 2015-10-16T16:51:44Z - The EFW (Electric Field and Waves) instrument consists of four orthogonal spherical sensors deployed from 50 m cable booms in the spin plane of the spacecraft, plus four deployment units and a main electronics unit. Each deployment unit deploys a multiconductor cable and tip-mounted spherical sensor. Each opposing pair of cables will be symmetrically deployed to a tip-to-tip distance of approximately 100 m, except for about a week at the beginning of the mission when 70 m will be used for one boom pair (the Z-booms) and 100 m for the other pair. The potentials of the spherical sensor and nearby conductors are controlled by the microprocessor to minimize errors associated with photoelectron fluxes to and from the spheres. Output signals from the sensor preamplifiers are provided to the wave instruments for analysis of high frequency wave phenomena. There is a 1 MB burst memory and tow fast A/D conversion circuits for recording electric field wave forms for time resolutions of up to 36,000 samples/s. Data gathered in the burst memory will be played back through the telemetry stream allocated to the instrument by pre-empting a portion of the real-time data. Incoming data are continuously monitored by algorithms in the software to determine whether to trigger the burst-playback mode. A large number of sampling modes is possible, yielding four possible telemetry rates from 1.440-29.440 Kbps. This data stream is transferred via the DWP instrument. The main measured quantities will be, in various modes: (1) the instantaneous spin-plane components of the electric field vector, from 0.1-700 V/Km, with time resolution down to 0.1 ms, in four frequency ranges from DC to upper limits of 10 Hz, 180 Hz, 4 KHz, or 32 KHz; (2) the AC electric field components from 10 Hz to 8 KHz, within the dynamic range of ~3 mV/Km to 10 V/Km; (3) plasma density fluctuations within the range of 1-100/cm and in three frequency ranges from 0 Hz to upper limits of 10 Hz, 180 Hz, or 4 KHz; and, (4) density and temperature (in Langmuir sweeps) in the eV range, with a dynamic range of 1-100/cm. There is also a frequency counter covering the range 10-200 KHz. On-board calculations of least-square fits to the electric field data over one spacecraft spin period (4 s) will provide a baseline of high-quality two-dimensional electric field components that are present in the telemetry stream, except for periods when three or four sensors are in current mode. The spacecraft potential is calculated and transmitted via DWP to other instruments on board. The three components from the search coil instrument (WHISPER) are also available in EFW with a bandwidth of 4 KHz. For more details of the Cluster mission, the spacecraft, and its instruments, see the report Cluster: mission, payload and supporting activities, March 1993, ESA SP-1159, and the included article The Spherical Probe Electric Field and Waves experiment for the Cluster Mission, by G. Gustafsson et al., from which this information was obtained. + Electric Field in ISR2 is obtained from CAA C[1-4]_CP_EFW_L3_E + + The EFW instrument measures the electric field only in the spacecraft + spin plane, therefore a spin-plane oriented coordinate system is best suited for scientific studies involving the electric field. The ISR2 (Inverted Spin Reference) system, also known as DSI (Despun System Inverted), is such a system. The X and Y axes are in the spin plane, with X pointing as near sunward as possible and Y perpendicular to the sunward direction, positive towards dusk. The Z-axis is along the (negative) spacecraft spin axis, towards the north ecliptic. The coordinate system is called Inverted because the actual spin axis of Cluster is pointing towards the south ecliptic. The difference between ISR2 (DSI) and the GSE (Geocentric Solar Ecliptic) is a tilt of 2° to 7° of the Z-axis performed in order + to avoid shading of the EFW probes by the spacecraft. NASA, Georg Gustafsson spase://SMWG/Person/Elena.Budnik @@ -19,8 +23,9 @@ This site provides information concerning the Cluster II Tango Electric Field and Waves Instrument. - spase://SMWG/Observatory/Cluster-Tango - ObservedBy + c4-efw-efield + PartOf + electric field @@ -71,7 +76,7 @@ magnetotail lobe - Duskward Electric Field Vector + e_sr2 c4_e_sr2 Cluster II Tango Prime Parameter Electric Field and Waves duskward electric field at spin time resolution phys.elecField @@ -80,7 +85,7 @@ 1.0e-3>V m^-1 Cartesian - GSE + SR2 TimeSeries @@ -93,18 +98,19 @@ c4_e_sr2(0) - ex + ey 2 c4_e_sr2(1) + -1.e9 Vector Electric - e_sr2_quality + e_quality c4_e_sr2_qual meta.code.qual PT4S diff --git a/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-pot-full.xml b/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-pot-full.xml index 8e8ae36..cebc889 100644 --- a/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-pot-full.xml +++ b/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-pot-full.xml @@ -21,7 +21,7 @@ c4-efw-pot PartOf - probe potential + s/c potential diff --git a/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-pot-spin.xml b/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-pot-spin.xml index 9a66b0f..4b868dc 100644 --- a/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-pot-spin.xml +++ b/NumericalData/AMDA/Cluster/Cluster4/EFW/clust4-pot-spin.xml @@ -21,7 +21,7 @@ c4-efw-pot PartOf - probe potential + s/c potential -- libgit2 0.21.2