Each unit is precision-calibrated and undergoes full-temperature compensation, along with qualification testing including thermal vacuum, EMC, magnetic, and total ionizing radiation dose tests. Designed for aerospace applications, it delivers reliable angular rate, temperature, and real-time diagnostic outputs in space environments.
Specifications
|
PRODUCT MODEL |
Units |
INT310Y |
|
MEMS Gyroscope |
||
|
Range |
/S |
±100/±100/±100 |
|
Bias |
°/h |
10/10/5 |
|
Bias Instability |
°/h |
0.5/0.1/0.03 |
|
Bias Stability Over Temperature (10s 1σ) |
°/h |
5/1/0.3 |
|
Bias Repeatability(1σ) |
°/h |
5/1/0.3 |
|
Angle Random Walk |
1 √h |
0.15/0.05/0.01 |
|
Scale Factor Nonlinearity |
ppm |
200/100/100 |
|
Scale Factor Repeatability |
ppm |
200/100/100 |
|
Orthogonality |
% |
0.1 |
|
Bandwidth |
Hz |
10 |
|
System Specifications |
||
|
Power Supply Voltage |
V |
+4.8~+6.0 |
|
Power Consumption |
W |
1.5 |
|
Dimensions(L x W x H) |
mm |
46×45×25 |
|
Weight |
g |
72±5 |
|
Operating Temperature |
℃ |
-40~+70 |
|
start-up time |
S |
1 |
|
Output Frequency |
Hz |
Supports Blind Sending Supports Polled Mode Output |
|
Interface |
||
|
Electrical Interface |
|
RS422×1 |
|
Connector |
|
J30J-15ZK |
Application
- Commercial aerospace
- Commercial sat
- Cargo spaceship
- ＜800km LEO
