µADC Models
Aeroprobe’s Micro Air Data Computers (μADC) are a critical component of the aircraft avionics system. Optimized for use on Uncrewed Aerial Vehicles, they provide real-time measurement of airspeed, altitude, angle-of-attack, and angle-of-sideslip which the flight control unit or pilot use to conduct the mission efficiently and safely. Each model was designed for a specific mission profile to meet the aggressive performance requirements of your aircraft. Choose the right model for your mission.
Aeroprobe offers seven μADC models well-suited for a wide variety of applications.
Pitot-Static Probe Compatible Micro Air Data Computers
| Atlas |  |
Extended velocity range 162 grams |
| Horizon | |
Extended velocity range 178 grams |
Industry Applications
Aerospace
Motor Sports
Unmanned Systems
Wind Power
Probes
Air Data
Heated Air Data
Pitot-Static
Case Studies
Area I
Atmospheric Research
Dream Chaser
Flight Characterization
Air Data Probe (ADP) Compatible Micro Air Data Computers
| Defiant |  |
+/- 20° AoA & AoS angle range 181 grams |
| Hyperion |  |
+/- 20° AoA & AoS angle range 192 grams |
| Athena | |
+/- 20° AoA & AoS angle range 200 grams |
| Endurance | |
+/- 40° AoA & AoS extended angle range 193 grams |
Certified Reliability
In addition to being lightweight and cutting-edge, our products are also reliable and expertly engineered. Our µADCs have achieved certifications from independent labs that demonstrate their ability to be operated in harsh conditions, including extreme temperature and vibration environments. Additionally, add-on testing is available for application-specific needs. The fourth generation µADC models have achieved MIL-STD 810H and RTCA DO-160G certifications, which include:
- Storage & Short-Term Op. High Temperature
- Operational High Temperature
- Storage & Operational Low Temperature
- Cyclic Temperature & Altitude
- Vibration
- Shock
Fourth Generation μADS Specifications:
Third Generation µADS Specifications
Accessories include a bench-top testing cable. The cable facilitates testing of all the μADC functions in a lab environment before integrating into the aircraft or platform.
