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.«

c-astral-orthophoto

»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 Take-Off

Autonomous Catapult TakeOff

/Users/Nejc/C-ASTRAL/C-Astral 2011/WEBSITE/ortofoto_sistem.dwg

Typical flight procedure

Parachute landing

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.

Ortophoto gallery samples

Ortophoto gallery samples

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
FLIGHT
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
SENSOR INFO
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