Each unit undergoes precision calibration, full-temperature compensation, and rigorous aerospace-standard screening, along with qualification tests including thermal vacuum and EMC. Designed for space applications, it provides stable angular rate, temperature, and real-time diagnostic outputs in orbital environments.
Specifications
|
PRODUCT MODEL |
Units |
EX300Y |
|
MEMS Gyroscope |
||
|
Range |
°/s |
±100 |
|
Bias |
°/h |
3 |
|
Bias Instability |
°/h |
0.03 |
|
Bias Instability (10s, 1σ) |
°/h |
0.3 |
|
Bias Instability (100s, 1σ) |
°/h |
0.15 |
|
Bias Repeatability(1σ) |
°/h |
0.2 |
|
Angle Random Walk |
1 √h |
0.02 |
|
Scale Factor Nonlinearity |
ppm |
100 |
|
Scale Factor Repeatability |
ppm |
100 |
|
Cross-Coupling |
% |
0.1 |
|
Bandwidth |
Hz |
10 |
|
System Specifications |
||
|
Power Supply Voltage |
V |
4.8~5.6 |
|
Power Consumption |
W |
6.5 |
|
Dimensions(L x W x H) |
mm |
85×85×61 |
|
Weight |
g |
<510 |
|
Operating Temperature |
℃ |
-40~+70 |
|
start-up time |
S |
2 |
|
Output Frequency |
Hz |
Supports Blind Sending Supports Polled Mode Output |
|
Interface |
||
|
Electrical Interface |
|
RS422×1 |
|
Connector |
|
J30J-25ZK |
Application
- Commercial aerospace
- Commercial sat
- Cargo spaceship
- ＜800km LEO
