System
»Bramor gEO, Advanced & Reliable mapping solution«
The BRAMOR gEO UA (unmanned aerial) SYSTEM, ideally suited for remote sensing GIS applications is comprised of a blended wing body modular airframe, with the emphasis on the smallest possible T/O weight, advanced aerodynamics, electric propulsion, completely autonomous operation, endurance, turbulent air penetration and stability, ergonomic and user friendly ground control station, durability and mobility. The airframe is made of advanced composite materials (Kevlar/Carbon/Vectran) that provide a high level of survivability. A high visibility color scheme, strobe and NAV lights are optional. Embedded autonomous flight procedures include an array of fail-safe options based on man-rated standards.
The system consists of the air vehicle with a 24.3Megapixel COLOR or INFRARED sensor, a foldable portable takeoff catapult and rugged ground control station. The whole system fits into two rugged transport cases or a single backpack. The system is flight ready in under five minutes and safely operated by single operator/pilot in command.
Equipped with C-Astral high rate GPS and GYRO precision data-logging electronics.
Your processing time will be shortened by the ability to acquire same amount of data and consistent overlaps when flying against or with the wind!
»Directly compatible with EnsoMOSAIC, PIEneering, Pix4D, Agisoft Photoscan, Menci Software, or other GIS image processing software solutions.«

»Autonomous takeoff, autonomous flight and parachute landing«
Bramor UAS is easy to use; autonomous / automatic takeoff procedure (no manual operation needed) and parachute landing enable ease of use. Training for operators/pilots is short.

Autonomous Catapult TakeOff

Typical flight procedure

Automated parachute landing
»1,29cm/pixel at 100m AGL !!!«
Use Bramor gEO for unprecedented precision and reliability of your own ortophoto data-sets high precision DSM’s and Pointclouds.
Technical data
AIRFRAME| Wingspan | 230 cm |
| Platform length | 96 cm |
| Center module length | 67 cm |
| Wing area | 67 dm2 |
| Engine | Brushless |
| Onboard power | li-po |
| T/O Weight | 3,8 kg |
| Max T/O weight | 4,0 kg |
| Optimal cruise speed | 16m/s |
| Max horizontal speed | 23m/s |
| Takeoff speed | 15-16m/s |
| Stall speed | 12-13m/s |
| Endurance | Up to 100 min |
| Command & control RF | 868 MHz or 900 MHz + options |
| Command & control range | Up to 40 km |
| Takeoff | Autonomous / catapult |
| Navigation | Autonomous / waypoints array |
| Landing | Autonomous / parachute |
| Emergency failsafe’s | User-Pre-program |
| DSLR camera resolution | 24.3 MP (1.29cm/pixel at 100m AGL) GSD |
| Onboard storage | SD Card |
| Onboard precision telemetry | Space separated values |
| Lens type | 30mm F2.8 |
| Image overlap | Custom X and Y |
| Photo trigger | Automatic at waypoint |
| Maximum operational wind speed | 13m/s demonstrated |
| Typical flight altitude AGL | 40-4300m ASL |








