| Key Features |
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Increased cross-wind takeoff and landing performance: 25+ kts demonstrated |
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Increased rate-of-climb and descent: 1500 fpm/6000 fpm |
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Increased maneuverability and g-loading: rated to +12 G’s |
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Wider range of speeds: 70 - 215 kts |
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Higher useful payload/total weight ratio: 1000 lbs load/3000 lbs MGTOW |
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FAA-certified, general aviation powerplant: Lycoming 185hp IO-360 |
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The Mobius™ Optionally Piloted Aircraft (OPA) system is designed to fulfill a wide range of unmanned ISR and RSTA missions. The aircraft can also be flown in a manned configuration providing flexibility for operations, training, and R&D. Open architecture across the entire system design assures maximum operational flexibility.
The Aircraft & Key Components
Based on a proven, FAA-certificated design (Experimental R&D Certificate), the carbon-composite aircraft overcomes many of the operational and logistical limitations of more classic, glider-like designs found in nearly all of today’s unmanned aircraft. |
| View Data Sheet |
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| Adobe .pdf 704 KB |
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