MAGSAT MAGNETIC FIELD DATA INTRODUCTION This directory contains half-second resolution magnetic field vectors from NASA's MAGSAT spacecraft (300-600 km altitude, 90 deg inclination) taken between November 2, 1979 and May 6,1980. DESCRIPTION OF THE DATA The MAGSAT project objectives were: - to obtain accurate vector measurements of the near-Earth geomagnetic field; - to use those measurements to identify and model the main (core) and crustal fields; - to study of fields from external sources. The data consist of position data for the MAGSAT spacecraft, and 0.5 s resolution observations from the MAGSAT triaxial fluxgate magnetometer (Dr. Robert A. Langel, NASA/GSFC, Principal Investigator). These data have been extracted from the original 1/16-second CHRONFIN data tapes archived at the NSSDC. The geomagnetic field data are given as Cartesian components in a NEV (North, East, Vertical) geocentric spherical coordinate system. In this system, the V component is positive directly towards the Earth's center. The N and E components are positive northward and eastward. The N and V components are defined relative to geocentric circles, and not relative to geodetic ellipsoids relative to which ground- observatory-measured geomagnetic BX, BY, and BZ are defined. Use of `BX,BY BZ' in this documentation refer to BN, BE, BV, and not to the (BX,BY,BZ) defined relative to an ellipsoid. Spacecraft position data are also given relative to a geocentric spherical system rather than to ellipsoidal coordinates. See [1] for a discussion of the differencies between the coordinate systems as applied to field data and spacecraft position data (also see below), and for a discussion of MAGSAT data and of the International Geomagnetic Reference Field. Fluxgate magnetometers are subject to drift, although inflight calibration with the MAGSAT cesium scalar magnetometer largely compensated for these drifts. Spacecraft attitude was measured with a combination of star trackers and sun sensor. Small shifts in attitude are detectible during the field modeling process. Afte inflight calibration, the vector measurements are thought to be accurate to a 1-sigma value of 3 nT. Users of the data should note that because of imperfect calibration of the attitude determination system, there are numerous small jumps in the component data (not in the corresponding magnitude data). The MAGSAT position accuracy is believed to be 60 meters radially and 300 meters horizontally. Note that MAGSAT moved at about 8 km/s in its orbit. MAGSAT FORMAT Logical record: 64 bytes + CR/LF for ASCII files. ========================================================================== Item Description Binary ASCII Units Notes ========================================================================== 1 Milliseconds of day I*4 I8 millisec 2 LAMBDA Geocentric R*4 F8.3 degree -90.000 - 90.000 latitude of spacecraft 3 PHI Geocentric R*4 F8.3 degree -180.000 - 180.000 longitude of spacecraft 4 R Radial distance R*4 F9.3 km 6670 - 7000 from center of the Earth to spacecraft 5 BX Geocentric R*4 F8.1 nT North component of magnetic field 6 BY Geocentric R*4 F8.1 nT East component of magnetic field 7 BZ Geocentric R*4 F8.1 nT vertical component of magnetic field 8 Atitude processing I*4 I5 flag [2] ========================================================================== REFERENCES 1. R. A. Langel, International Geomagnetic Reference Field: The Sixth Generation, J. Geomag. Geoelectr, 44, 699-702, 1992. 2. R. Langel, J.Berbert, T.Jennings, and R.Horner, Magsat data processing: a report for investigators, NASA Technical Memorandum 82160, November 1981, GSFC (Available from NSSDC).