Inertial Measurement Units

20 Inertial Measurement Units for Space Applications from 10 manufacturers listed on SatNow

Inertial Measurement Units for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

Description:Very High-Performance Fog Fibre Optic Inertial Measurement Unit
Orbit:
GEO, LEO, MEO
Input Voltage:
22 to 50 V
Power Consumption:
6 W
Dynamic Range:
±10 Degree/Sec, Up to ±140 Degree/Sec
Angular Random Walk:
0.0016 Degree/vh
Bias Stability:
0.01 Degree/hr
Alignment Stability:
130 µrad (Absolute), 200 µrad (Relative)
Scale Factor Stability:
10 ppm (1 Month), 200 ppm (5 Years)
Mass:
6.5 Kg (ICU 2 kg, GEU 4.5 kg)
Vibration:
25 g (Sine), 16 grms (In Plane), 23 grms (Out of p...
Radiation Tolerance:
50 krad
Interface:
RS-422
Space Heritage:
Yes
more info
Description:Strategic-Grade, Cost-Effective, Next-Generation Fiber Optic Gyros (FOGs)
Angular Random Walk:
100 µ Degree/vhr
Interface:
RS-422
more info
Description:Miniature Inertial Measurement Unit for Satellite and Deep Space-Probe Applications
Input Voltage:
28 to 100 V
Power Consumption:
25 to 32 W
Dynamic Range:
±375 Degree/Sec
Angular Random Walk:
0.005 Degree/vh
Bias Stability:
0.02 Degree/hr
Scale Factor Stability:
1 ppm (Per Year)
Mass:
4.6 to 4.7 Kg
Vibration:
19.7 grms
Radiation Tolerance:
100 krad
Interface:
RS-422
more info
Description:Inertial Fiber-Optic Gyro For Space Applications Small, Lightweight, Highly Reliable, State Of The Art Inertial Measurement Unit (Imu)
Input Voltage:
5 to 15 V
Power Consumption:
4 W
Dynamic Range:
1000 Degree/Sec
Angular Random Walk:
0.07 Degree/vh
Bias Stability:
1 Degree/hr
Alignment Stability:
0.1 mrad
Scale Factor Stability:
100 ppm
Mass:
0.748 Kg
Vibration:
15 grms
Data Rate:
400 Hz
Radiation Tolerance:
10 krad
Interface:
RS-422, RS-485
Space Heritage:
Yes
more info
Description:Complete Small Satellite based inertial sensor technology into inertial measurement units (IMUs)
Satellite Type:
SmallSat
Input Voltage:
5 to 12 V
Power Consumption:
0.6 W
Dynamic Range:
0.2 Degree/Min
Mass:
0.02 Kg (Without Enclosure), 0.06 Kg (With Enclosu...
Interface:
RS-485
more info
Description:3 Axis Fiber Optical Gyro Unit For Micro-Satellite
Satellite Type:
MicroSat
Input Voltage:
15 to 28 V
Power Consumption:
3.5 W
Dynamic Range:
±5 Degree/Sec, ±10 Degree/Sec
Bias Stability:
1.73 Degree/hr, 5 Degree/hr
Mass:
1.2 Kg
Interface:
RS-422
Space Heritage:
Yes
more info
Description:MEMS-based gyros, 3 high stability accelerometers and 3 high stability inclinometers IMY in a miniature package
Input Voltage:
5 V
Power Consumption:
1.8 to 2.5 W
Dynamic Range:
400 Degree/Sec
Angular Random Walk:
0.15 Degree/vh
Bias Stability:
0.3 Degree/hr
Scale Factor Stability:
50 to 400 ppm
Radiation Tolerance:
48 to 125 krad
Interface:
RS-422
more info
Description:The Latest Closed-Loop Fiber-Optic Gyro (Fog) And Linear Rebalanced Accelerometer Technology
Input Voltage:
5 to 15 V
Power Consumption:
15 W
Dynamic Range:
±1000 Degree/Sec
Angular Random Walk:
0.07 Degree/vh
Bias Stability:
1 Degree/hr
Scale Factor Stability:
100 ppm
Mass:
0.84 Kg
Data Rate:
100 to 4800 Hz
Interface:
RS-422
Space Heritage:
Yes
more info
Description:ITAR-free, Single Event Latch-up tolerant and high-performance Inertial Measurement Unit
Orbit:
LEO
Input Voltage:
15 V
Power Consumption:
10 W
Dynamic Range:
±400 Degree/Sec
Angular Random Walk:
0.01 Degree/vh
Bias Stability:
0.3 Degree/hr, 1 Degree/hr (BOL)
Scale Factor Stability:
500 ppm
Mass:
2 Kg
Vibration:
14.5 grms
Data Rate:
200 Hz
Interface:
RS-422
more info


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