Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

Polar

Polar [NASA]

Polar is one of four spacecraft in the Global Geospace Science (GGS) program. These are among the spacecraft (Wind, Geotail, SOHO, and Cluster) in the International Solar Terrestrial Physics (ISTP) program. POLAR measures solar wind entry, ionospheric output, and the depositions of energy into the neutral atmosphere at high latitudes.

Imaging instruments make possible the measurement of visible, ultraviolet, and X-ray spectra of the polar caps. POLAR has on-board propulsion systems and a design lifetime of three to five years, with redundant subsystems. POLAR is cylindrical, approximately 2.8 m in diameter by 1.25 m high (plus 1.25 m for its two despun platforms), with body-mounted solar cells, weighs 1250 kg and uses 333 W of power. The spin rate is 10 rpm around an axis approximately normal to the orbital plane. It has long wire spin-plane antennas, inertial booms, and spin-plane appendages to support sensors. POLAR has two despun gimballed instrument platforms, and booms are deployed along both Z axes. Data are stored using on-board tape recorders and are relayed to the Deep Space Network at a high rate (600 kbps maximum, 250 kbps nominal), although the average real-time data rate for POLAR is 41.6 kbps. POLAR is placed in a 22.6-h polar orbit (90 deg inclination), with perigee and apogee of 11,500 and 57,000 km.

Following instruments were on board the spacecraft:

  • Toroidal Imaging Mass-Angle Spectrograph (TIMAS)
  • Plasma Waves Investigation (PWI)
  • Hot Plasma Analyzer (Hydra)
  • Comprehensive Energetic-Particle Pitch-Angle Distribution (CEPPAD)
  • Charge and Mass Magnetospheric Ion Composition Experiment (CAMMICE)
  • Polar Ionospheric X-ray Imaging Experiment (PIXIE)
  • Electric Fields Investigation (EFI)
  • Ultraviolet Imager (UVI)
  • Visible Imaging System (VIS)
  • Thermal Ion Dynamics Experiment (TIDE)
  • Magnetic Fields Experiment (MFE)

Polar was decommissioned in April 2008 after 12 years of service.

Nation: USA
Type / Application: Scientific
Operator: NASA
Contractors: Lockheed Martin Astro
Equipment: TIMAS, PWI, Hydra, CEPPAD, CAMMICE, PIXIE, EFI, UVI, VIS, TIDE, MFE
Configuration:
Propulsion:
Power: Solar cells, batteries
Lifetime: 2 years (planned), 12 years reached
Mass:
Orbit: 185 km × 50551 km,85.9
Satellite COSPAR Date LS Launch Vehicle Remarks
Polar 1996-013A 24.02.1996 Va SLC-2W Delta-7925-10

References:

  • NSSDC Master Catalog: Polar
Further ISTP missions: