Simulate high-altitude low-pressure environments for evaluating UAV avionics, brushless propulsion, and sensors.
Barometric altimeter calibration and GPS/INS sensor verification.
Thrust measurement and heat dissipation in thin air.
Thermal runaway, cell venting, and capacity discharge under vacuum.
Lens fogging, thermal stabilization, and actuator torque testing.
| Altitude Range | Ground level to 75,000+ ft (Down to ~25 mbar absolute pressure) |
|---|---|
| Temperature Range | -65°C to +120°C (Cascade refrigeration system with uniform airflow) |
| Chamber Volume | From 1,000 Litres (Avionics) to 25,000 Litres (Full UAV Airframe) |
| Observation Windows | Heated multi-pane optical glass for high-speed camera tracking |
| Telemetry Feedthroughs | Sub-D, BNC, Ethernet, CAN-bus, High-power DC electrical pass-throughs |
| Telemetry Software | Automated climb/dive profile simulation with real-time graph logging |
Direct consultation with our senior engineering team in Delhi.