The magnetometer on the POLAR Spacecraft is a high precision instrumen
t designed to measure the magnetic fields at both high and low altitud
es in the polar magnetosphere in 3 ranges of 700, 5700, and 47000 nT.
This instrument will be used to investigate the behavior of field-alig
ned current systems and the role they play in the acceleration of part
icles, and it will be used to study the dynamic fields in the polar cu
sp, magnetosphere, and magnetosheath. It will measure the coupling bet
ween the shocked magnetosheath plasma and the near polar cusp magnetos
phere where much of the solar wind magnetosphere coupling is thought t
o take place. Moreover, it will provide measurements critical to the i
nterpretation of data from other instruments. The instrument design ha
s been influenced by the needs of the other investigations for immedia
tely useable magnetic field data and high rate (100+ vectors s(-1)) da
ta distributed on the spacecraft. Data to the ground includes measurem
ents at 10 vectors per second over the entire orbit plus snapshots of
100 vectors per second data. The design provides a fully redundant ins
trument with enhanced measurement capabilities that can be used when a
vailable spacecraft power permits.