• Endurance: 25–40 minutes @ MSL.
• Range (LoS): 2–4 km.
• Weight: < 3.5 kg.
• Wind Resistance: Up to 20 knots or 36 km/h.
• Max Operating Altitude: Up to 400 m AGL.
• Max Launch Altitude: 3000 m AMSL.
• Vehicle Size: < 1 m x 1 m.

Operational Characteristics:

• Launch & Recovery- Autonomous Vertical Take-Off and Landing (VTOL)
• Maximum space required for recovery: 25mX25m open area

Flight Modes:

• Fully autonomous from Take-Off to Landing without using any R/C controller.
• Altitude hold.
• Autonomous waypoint navigation (pre-defined as well as dynamically adjustable waypoints during flight times).

Deployment time (from fully packed state to UAV Taker –Off): <10 minutes.

Packing Time (after UAV landing to fully packed state): <10 minutes.

Fail Safe Features:

• Return to home on communication failure.
• Return to Home/Land on low battery.
• Multiple GPS on-board for GPS failure redundancy.
• High wind indication.

Packaging and Storage: Hard case for transportation and storage.

Operating crew: Maximum 2.

Communication Link Characteristics:

• Transmit control commands from GCS to UAV.
• Transmit telemetry data from UAV to GCS.

Frequency Band: 2.4 GHz to 5 GHz.

Ground Control Station Characteristics:

• Laptop (Windows OS with Bluefire patented software).
• GUI Display Parameters: Geographic map along with UAV location, UAV trajectory, camera view polygon, waypoints and Flight plans.
• Artificial Horizon indicating UAV altitude.

Maps:

• Capability to works with Google maps and/or other available open source maps. Application should have
  the capability to download maps automatically after specifying the location GPS co-ordinates.
• Capability to integrate geo-referenced raster maps provided in at least one of the commonly used digital maps format. (gif, tiff etc.).

User Controls:

• One click Take-Off/Land/Hover.
• Set altitude of UAV.
• Waypoint navigation.
• Dynamic flight plan adjustment.
• Point payload to ground co-ordinate function.

Joystick control:

• RPV mode.
• Altitude control.

Pre Flight checks: Capability to perform pre-flight checks of the complete system before every flight for confirming the suitability of flight worthiness.

Payload: 

• Thermal Payload (Black/White hot): 320 x 240 pixels, 640 × 480 pixels (Optional).
• Thermal Payload: 640 × 480 pixels (Radiometric).