| Power Plant: |
26cc 2-stroke engine |
| Fuel: Gasoline |
JP-8, Jet-A, pump diesel, or kerosene
with a 50:1 oil mix |
| Dimensions: |
6 x 4 x 1.25 feet assembled
3.5 x 1.25 x 1.5 packed |
| Weight: |
22.0 lbs with standard tanks full fuel and payload |
| Speed: |
25 – 65 mph |
| Duration: |
6 hours (8 hours with optional wing fuel tanks) |
| Ceiling: |
9500 feet |
| Range: |
180 miles @ average cruise speed of 35 mph (fuel limit standard tanks)
7 miles radius limited by standard live telemetry link |
| Sensors: |
Sony HAD color video camera with variable 25x zoom
480 lines resolution. 3-axis gimbaled camera mount guided
by flight computer for geo-referenced imagery.
Optional thermal IR camera available |
| Payload: |
Additional 2.5 lbs with standard sensor package
Additional 5.0 lbs. without standard sensor package |
| Data Link: |
2.4 GHz video downlink standard
900 MHz 2-way modem standard
72 MHz uplink remote control standard |
| Launch: |
Hand launch or bungee catapult |
| Guidance: |
Fully autonomous flight capability
Mission plan created with proprietary graphical user interface |
| Recovery: |
Aircraft can land on wheels autonomously in 100 x 50 meter clear area |
| Operational: |
Winds up to 25 knots, moderate precipitation |
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