This page summarizes information about the selected resource and its origin based on SPASE metadata.
SPASE version 2.0.0
This is an hourly resolution, merged magnetic field and plasma data set created at NSSDC for COHOWeb. Magnetic field vectors and plasma flow direction angles are given in RTN coordinates. Spacecraft position data are given in Heliographic inertial (HGI coordinates).
Please acknowledge N.F. Ness (P.I.) and F. Mariani for magnetic field data and H. Rosenbauer (P.I.) and R. Schwenn for plasma data, and NSSDC or GSFC-SPDF
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Dr. Norman F. Ness |
| 2. | Principal investigator | Dr. Helmut R. Rosenbauer |
| 3. | CoInvestigator | Prof. Franco Mariani |
| 4. | CoInvestigator | Dr. Rainer Schwenn |
| 5. | General contact | Dr. Natalia E. Papitashvili |
for annual files via ftp
Helios 1-specific page for plots and lists
Plots, lists, scatter plots, regressions, distributions, means, etc.
Please acknowledge N.F. Ness (P.I.) and F. Mariani for magnetic field data and H. Rosenbauer (P.I.) and R. Schwenn for plasma data, and NSSDC or GSFC-SPDF
Plasma data end on day 364 of 1980.
Four digit Year
Decimal Day of Year
Hour
Carrington Rotation Number seen by an Earth based observer at the start of the data interval
Heliocentric radial distance of Helios 1 in AU
Heliographic Inertial elevation angle of Helios 1 in deg
Heliographic Inertial azimuthal angle of Helios 1 in deg
Earth-Sun-Spacecraft separation angle
Hourly averages of SSE (spacecraft-centric solar ecliptic) components of fine time scale magnetic field vectors
X,Y,Z components
| Index | Name | Component | Parameter key |
|---|---|---|---|
| 1 | X component | I | Column09 |
| 2 | Y component | J | Column10 |
| 3 | Z component | K | Column11 |
Hourly averages of RTN components of fine time scale magnetic field vectors
R,T,N components
| Index | Name | Component | Parameter key |
|---|---|---|---|
| 1 | R component | I | Column12 |
| 2 | T component | J | Column13 |
| 3 | N component | K | Column14 |
Hourly average of fine time scale magnetic field magnitudes
Hourly averaged solar wind plasma flow speed
Hourly averaged solar wind plasma flow elevation angle
Hourly averaged solar wind plasma flow azimuthal angle
Hourly averaged solar wind plasma density
Hourly averaged solar wind plasma temperature (radial component)
SPASE version 2.0.0
The E1 plasma experiment aboard the Helios solar probes consists of four independent instruments designed to investigate the solar wind plasma. By measuring the velocity distribution functions of the different kinds of particles, all important hydrodynamic parameters of the solar wind plasma can be derived. Three instruments (I1a, I1b, and I3) analyze the positive components (protons and heavier ions with energy-per-charge values from 0.155 to 15.32 kV) of the solar wind. Two of them allow for an angular resolution in both directions of incidence. The experiment employed a combination of a hemispherical, a quadrispherical, and a sinusoidally-shaped electrostatic analyzer.
All detectors were mounted normal to the spin axis.
One instrument (I2) measures electrons in the energy range from 0.5 the 1660 eV with one-dimensional angular resolution using a hemispherical electrostatic analyzer.
For more detailed information see p. 226 of Raumfahrtforschung, v. 19, n. 5, 1975.
User will acknowledge the Helios 1 Plasma Experiment PI F. H. R. Rosenbauer in any publication resulting from the use of these data.
| Role | Person | |
|---|---|---|
| 1. | Data producer | Dr. Rainer Schwenn |
| 2. | Principal investigator | Dr. Helmut R. Rosenbauer |
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This experiment (E3) consisted of a boom-mounted, triaxial-fluxgate magnetometer. An automatic inflight range switch system selected the optimum of four ranges that were minus to plus 16, 48, 144, and 432 nT per sensor. These had corresponding digitization resolutions of minus to plus 0.03, 0.09, 0.28, and 0.84 nT, respectively. A sensor flipper was actuated every 36 h to assist in sensor zero level determination. For telemetry bit rates above 256 bps, vector measurements were made at rates between 1 and 16 per s, depending on bit rates. At lower bit rates, averages and variances were computed on board for transmission to earth.
Information about the Fluxgate Magnetometer for Average Fields experiment on the Helios-A mission.
| Role | Person | |
|---|---|---|
| 1. | Principal investigator | Dr. Norman F. Ness |
SPASE version 2.0.0
This spacecraft was one of a pair of deep space probes developed by the Federal Republic of Germany (FRG) in a cooperative program with NASA. Experiments were provided by scientists from both FRG and the U.S. NASA supplied the Titan/Centaur launch vehicle. The spacecraft was equipped with two booms and a 32-m electric dipole. The payload consisted of a fluxgate magnetometer; electric and magnetic wave experiments, which covered various bands in the frequency range 6 Hz to 3 MHz; charged-particle experiments, which covered various energy ranges starting with solar wind thermal energies and extending to 1 GeV; a zodiacal-light experiment; and a micrometeoroid experiment. The purpose of the mission was to make pioneering measurements of the interplanetary medium from the vicinity of the earth's orbit to 0.3 AU. The spin axis was normal to the ecliptic, and the nominal spin rate was 1 rps. The outer spacecraft surface was dielectric, effectively (because of the sheath potential) raising the low-energy threshold for the solar wind plasma experiment to as high as 100 eV. Also, sheath-related coupling caused by the spacecraft antennae produced interference with the wave experiments. The spacecraft was capable of being operated at bit rates from 4096 to 8 bps, variable by factors of 2. While the spacecraft was moving to perihelion, it was generally operated from 64 to 256 bps; and near 0.3 AU, it was operated at the highest bit rate. Because of a deployment failure of one axis of the 32-m, tip-to-tip, dipole antenna, one axis was shorted, causing the antenna to function as a monopole. The major effect of this anomaly was to increase the effective instrument thresholds, and to introduce additional uncertainties in the effective antenna length. Instrument descriptions written by the experimenters were published (some in German, some in English) in Raumfahrtforschung, v. 19, n. 5, 1975.
Information about the Helios-A mission
| Role | Person | |
|---|---|---|
| 1. | Project scientist | Dr. James H. Trainor |
| 2. | Project scientist | Dr. Herbert Porsche |
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Space Physics Data Facility
Space Physics Data Facility
| Role | Person | |
|---|---|---|
| 1. | General contact | Ms. Tamara J. Kovalick |
| 2. | Technical contact | Mr. Robert M. Candey |
| 3. | Project scientist | Dr. Robert E. McGuire |