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| Categories | Accelerometers |
|---|---|
| Description: | Accelerometers RoHS |
| Mfr. Part #: | SCH16T-K01-10 |
| Model Number: | SCH16T-K01-10 |
| Company Info. |
| Changsha Purple Horn E-Commerce Co., Ltd. |
| Verified Supplier |
| View Contact Details |
| Product List |
The SCH16T-K01 is a high-performance 3-axis angular rate sensor and 3-axis accelerometer, utilizing Murata's proven capacitive 3D-MEMS technology. It features a mixed-signal ASIC for signal processing, providing angular rate and acceleration data via a flexible SafeSPI v2.0 digital interface. Packaged in a pre-molded SOIC 24-pin plastic housing, it ensures reliable operation and offers high stability, reliability, and quality. The component exhibits stable output across temperature, humidity, and vibration, and includes advanced self-diagnostic features. It is suitable for SMD mounting and compliant with RoHS and ELV directives.
| Feature | Details |
|---|---|
| Gyroscope Measurement Range | Selectable in-application from 300 /s down to 62.5 /s |
| Accelerometer Measurement Range | Selectable in-application from 80 m/s down to 15 m/s (typical default dynamic range up to 260 m/s) |
| Output Options | Interpolation and decimation |
| Low Pass Filters | 13Hz to 370 Hz cut-off rate for angular rate and acceleration |
| Synchronization Features | Data Ready output, timestamp index, SYNC input |
| Operating Temperature Range | -40...110 C |
| Supply Voltage | 3.0...3.6 V (main), 1.73.6 V (I/O) |
| Digital Interface | SafeSPI v2.0 |
| Output Data Resolution | 20-bit and 16-bit (selectable via SPI frame) |
| Self-Diagnostic Features | Extensive, utilizing over 200 monitoring signals |
| Package | SOIC-24 (11.8 mm x 13.4 mm x 2.9 mm) |
| Qualification | AEC-Q100 standard |
| Sensor Type | 6-DOF XYZ-Axis gyroscope and XYZ-Axis accelerometer |
The SCH16T-K01 is designed for applications requiring high performance under demanding environmental conditions, including: Inertial measurement units (IMUs), Inertial navigation and positioning, Machine control and guidance, Dynamic inclination, Robotic control and UAVs.
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