Stork Agriconnaisance
Flight system
| Wingspan | 3,3 m | |
| Length | 1,03 m | |
| Airframe material | full composite and carbon with carbon kevlar strenghtening | |
| Flight-ready mass of airframe without fuel | 8 kg | |
| Maximum takeoff weight | 20 kg | |
| Payload | 6-7 kg | |
| Drive | electric engine | |
| Maximum power | 1,9 Kw | |
| Takeoff | catapult | |
| Landing | belly landing or parachute | |
| Flight time | 3 – 4 hours | |
| Range | maximum 300 km | |
| Cruising speed | 21m/s | |
| Minimum speed (with open flaps) | 11m/s | |
| Maximum speed | 44m/s | |
| Control system | 2,4 GHz, 5 GHz, 4G GSM, using short wave and satellite channels optionally according to areal regulations; purpose driven and/or directly controlled system, capable of autonomous flight and activating high level safety protocols; redundant autopilot system with independent assessing and decision-making electronic solutions. Smart flight controller case with isolated screens and joysticks for surveillance and control tasks. 01, lux luminance integrated pilotcamera independent of surveillance tasks |
Surveillance system
Camera
Multispectral camera
Sensor & Lens Parameters
The values shown at right were derived from the FOV (Field of View) Optical Calculator contained in Tetracam’s PixelWrench2 software (included with all Micro-MCA cameras) using the current values for the Micro-MCA camera shown below:
Sensor Dimensions (mm): 6.66 x 5.32
Pixel Size (microns): 5.2
Camera Lens Focal Length (mm): 9.6
| Object Distance(Altitude Above Ground Levelin meters) | Ground Resolutionin mm per pixel | FOV (width x height) in meters |
| 122 m (~ 400 ft) | 66 | 84×67 |
| 213.4 m (~ 700 ft) | 116 | 148×118 |
| 365.8 m (~ 1200 ft) | 198 | 254×203 |
| 915 m (~ 3000 ft) | 496 | 635×508 |
Data transmission services
- Encrypted data transmission system, real time video feed within 40 km radius from the flight control case