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 Bear (P87-1)

Polar Bear [APL]

Polar Bear (Polar Beacon and Research), also known as STP P87-1, was a military mission designed to study communications interference caused by solar flares and increased auroral activity.

It was to continuie the mission of its predecessor, HILAT. The spacecraft was built on the Transit-O 17 navigational satellite that was retrieved from the Smithsonian's National Air & Space Museum, where it had been on display for 8 years.

Polar bear was gravity gradient stabilized by deployable boom with tip mass and was powered by 4 small deployable solar arrays.

The payload consisted of:

  • Auroral Imaging Remote Sensor for aurora borealis imaging
  • Beacon Experiment to monitor ionospheric propagation over the poles

In November 1986, the satellite was launched on a Scout-G1 into orbit to measure the properties of the near-Earth plasma. However, as it entered its first period of fully sunlit orbit in February 1987, its attitude degraded significantly. The roll, pitch, and yaw angles began oscillating until the satellite finally inverted in May 1987. Consequently, several attempts to re-invert the satellite were undertaken. The third attempt proved to be successful when the momentum wheel was allowed to despin for an orbit before spinning it back to its maximum spin rate. The torque from the wheel in combination with the pitch rate induced from the despinning wheel inverted the satellite and captured it in the desired orientation.

Nation: USA
Type / Application: Experimental
Operator: USAF STP (Space Test Program)
Contractors: JHU/APL
Equipment: Auroral Imaging Remote Sensor, Beacon Experiment
Configuration: Transit-Bus
Propulsion: ?
Power: 4 deployable solar arrays, batteries
Lifetime:
Mass: 125 kg
Orbit: 955 km × 1013 km, 89.6
Satellite COSPAR Date LS Launch Vehicle Remarks
Polar Bear (P87-1) (ex Transit-O 17) 1986-088A 14.11.1986 Va SLC-5 Scout-G1 mod. Transit-O 17
Further STP missions: