OVERVIEW

ARIM310 is a small integrated probe capable of acquiring the following parameters:

• Barometric Pressure
• Pitot Pressure
• Angle-of-attack
• Angle-of-sideslip
• Temperature
• Humidity

The ARIM310 utilizes high-performance digital signal processing and all sensor correction model to reduce all sensor data in real-time by providing:

• Static Pressure – corrected for position error (Ps)
• Total Pressure (Pt)
• Indicated Air Speed (IAS) / Altitude (IA)
• Calibrated Air Speed – corrected for position error (CAS) / Altitude (CA)
• True Air Speed – corrected for position error (TAS) / Altitude (TA)
• Equivalent Air Speed (EAS) / Altitude (EA)
• Angle of Attack – corrected for position error (AOA)
• Angle of Sideslip – corrected for position error (AOS)
• Total Air Temperature (TAT)
• Outside Air Temperature – corrected for dynamic heating(OAT)
• Impact Pressure

The ARIM310 MEMS-based air-data and inertial sensors, and all analog and digital processing electronics are fully integrated into a small enclosure which can be easily mounted inside the fuselage of an airframe with the measurement boom protruding through the fuselage skin into the free stream flow, thereby providing an end-to-end measurement solution. Measured data is broadcast via a CAN Aerospace Serial Communications Interface.

SPECS

Please call us at (01) 705 722 4288 for technical specifications

DOWNLOADS

BROCHURES, USER MANUALS, AND ICDs

MECHANICAL DRAWINGS

• ARIM310 2D Drawing - Sheet 1 of 3.pdf
• ARIM310 2D Drawing - Sheet 2 of 3.pdf
• ARIM310 2D Drawing - Sheet 3 of 3.pdf

SPEC SHEETS

FIRMWARE

GALLERY