| Root mean square (RMS) error of initial heading angle determination, max, ° (1) | 0.085 / cos (geographic latitude) |
| RMS heading hold error over 1 hour of operation, max, ° (1) | 0.03 |
| RMS roll / pitch angle determination error, max, ° (1) | 0.04 (in motion) |
| RMS position dead-reckoning error with correction from an external speed sensor, % of travelled distance, max (2) | 0.3 |
| RMS position dead-reckoning error in autonomous (inertial) mode, km per flight hour, max (3) | 3.6 |
| Measurement range: pitch / roll, ° | ±90 / ±180 |
| Measurement range: heading, ° | 0…360 |
| Measured angular rate range: X/Y/Z, °/s | ±400 |
| Measured acceleration range: X/Y/Z (g) | ±18 |
| Operating temperature (endurance), °C | -40…+55 |
| Storage temperature (strength), °C | -50…+75 |
| Vibration (endurance) (random 100 Hz–1 kHz), g rms | 7 |
| Shock (strength), duration: 10 ms, waveform | 60 |
| Functional readiness time, max, s | 5 |
| Fast gyrocompassing time, max, s | 360 |
| Navigation solution rate, Hz | 610 (1220 on request) |
| Input / output interfaces | RS-232/422/485, Ethernet 100 Mbit, discrete signals |
| Supply voltage / power consumption | 18…32 V / max 20 W |
| Overall dimensions (L x W x H), mm, max | 160x170x180 |
| Weight, kg, max | 6 |
| Mean time between failures (MTBF) (calculated), h | 10 000 |