MRN-01 MRN-01 Small & redundant inertial sensor (IMU)

MRN-01 is composed of high precision MEMS gyroscopes and accelerometers and is redundant product by incorporating 2 IMU units

Description

  • Redundant IMU with 2 independent 3-axis IMU units
  • IMU for space is composed of high precision MEMS gyroscopes and accelerometers
  • Space environment resistant
  • Proven for long-term use in space

Application

MRN-01 is composed of high precision MEMS gyroscopes and accelerometers and is redundant product by incorporating 2 IMU units

  • Launch vehicle
  • Satellite
  • Rover
Item Value
MRN-01
Gyroscope Performance Measurement range ±400 deg/s
Performance range ±30 deg/s
Bias over temperature 10deg/h
Bias repeatability 20 deg/h
Bias instability 0.2 deg/h
Angle random walk 0.051 deg/√h
Scale factor over temperature 500 ppm
Scale factor non-linearity 500 ppm
Misalignment 4m rad
Bias vibration sensitivity 1 deg/h/grms²
Acceleration Performance Measurement range ±30 g
Performance range ±11 g
Bias over temperature 1 mg
Bias repeatability 3 mg
Bias instability 90 μG
Angle random walk 150 mm/s/√h
Scale factor over temperature 500 ppm(±3g)
Misalignment 4m rad
Bias vibration sensitivity 0.15 mg/grms²
Item Value
Electrical Characteristics Supply voltage 12VDC±1V
Power consumption 5W (2.5W/Unit)
Warm-up time 30min
Mechanical Characteristics Dimensions 153 × 106 × 83 mm
weight 1.3kg
Electrical interface Micro D-sub 15pin×2
Interfaces Data output cycle 100Hz
Output format RS422
Communication specification Asynchronous serial
Baud rate 115,200bps
Operating Conditions Operating temperature range -24℃~65℃
Performance temperature range -14℃~55℃
Humidity (operation) 60%RH
Random vibration(operation)
XY direction:112m/s² rms
Z direction:150m/s² rms
Low frequency shock(operation) 139m/s² × 10ms
High frequency shock(operation) 50~790 Hz: +6dB/oct
790~4000Hz: 3335m/s²
    

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