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The same inertial reference system is systems are installed permanently on Polar 5 and Polar 6.

|| Dimension Laseref KT19.85IIV (L x W x H)| 237165 x 66 163 x 138163 mm ||
|| Weight KT19.85II | 24.355 kg||
|| Power Supply| 22 - 30 VDC ||
|| Data interface | analog output (0-20mA) and serial interface (RS232)ARINC 429||

After the flight KT19.85IIINS data are accessible via the land system of the aircraft data managment system (DMS).

|| Module name| B839B700 KT19Avionics||
|| Device name | KT19Internal radiationNavigation thermometer analogSystem||
|| Parameters | CalibrationEast TemperatureWest RawVelocity \[Ohmknots\]; East West Velocity Status; ErrorText; Ground Speed \[knots\]; Ground Speed Status; Inertial Altitude \[fts\]; Inertial Status; Temperature Raw \[A\] ||
|| Device name | KT19 radiation thermometer serial||
|| Parameters | ErrorText; KT19 Serial;Altitude Status; Inertial Vertical Speed \[ft/min\]; Intertial Vertical Speed Status; Latitude \[deg\]; Latitude Status; Longitude \[deg\]; Longitude Status; Magenitc Heading \[deg\]; Magenitc Heading Status; North South Velocity \[knots\]; North South Velocity Status Pitch Angle \[deg\]; Pitch Angle Status; Pitch Rate \[deg/s\]; Pitch Rate Status; Roll Angle \[deg\]; Roll Angle Status; Roll Rate \[deg/s\]; Roll Rate Status; Status; True Heading \[deg\]; True Heading Status; True Track Angle \[deg\]; True Track Angle Status; Vertical Acceleration \[g\]; Vertical Acceleration Status; Wind Direction \[deg\]; Wind Direction Status; Wind Speed \[knots\]; Wind Speed Status; X Acceleration \[g\]; X Acceleration Status; Y Acceleration \[g\]; Y Acceleration Status; Yaw Rate \[deg/s\]; Yaw Rate Status; Z Acceleration \[g\]; Z Acceleration Status ||