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Micro Unmanned Aerial Vehicles |
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Prime Manu.
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UAV Designation
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| Development | Production | Operation | Purpose | Mission payload | Launch, take-off type | Recovery, landing type | Min ground crews need | System composite | Datalink, comm frequency | Engine | Power Sources | Propulsion | Surface | Wing span | Wing area (c§³) | Length overall | Height overall | Wheel track | Wheel base | Wing aspect ratio | Fuselage max width | Weight empty | Max fuel weight | Max payload | Max T-O/launch weight | Max level speed (kt) | Cruising speed (kt) | Loiter speed (kt) | Stall speed (kt) | Service ceiling (ft) | Max rate of climb (ft/min) | Max range (nm) | Max endurance (h) | ||||
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KOREA
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KIST |
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Underway | Reconnaissance MAV | Color CMOS video camera | 1.4 GHz | ICE(Cox 0.010 Tee Dee) | Fuel for glow engine | elevator | 26.65 | |||||||||||||||||||||||||||
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Spot |
Underway | Reconnaissance MAV | Color CMOS video camera | 2.4 GHz | Electric Motor using | Li-ion battery | elevator, rudder | 14.9 | 181.50 | 1.24 | wing loading 3.7 kg/§³ | 68.5 | 10 m/sec | ||||||||||||||||||||||||
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Seoul National University |
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Underway | Reconnaissance
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USA
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Aero Vironment
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Black Widow
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Underway | Underway | Micro UAV | Miniature black Color CMOS video camera, Two-axis magnetometer, Pitot-static tube, Piezoelectric-gyro, Autopilot(altitude hold, airspeed hold, heading hold, and yaw damping.) | Pneumatic launcher. | Belly landing. | Entire system ( air vehicles, launcher, controls, monitor and antenna) packaged in standard briefcase. | Autonomous navigation. | Hand-held proportional radio transmitter, antenna and TV monitor. | Electric motor, powered. | lithium batteries | A two-blade prop. | elevator, rudder | 15.24cm(6.0 in) | Structure: 10 Propulsion: 37 Controls: 6 | 7 | 60 | Dash speed: 39 | 23 | 1.8 | 30 min | ||||||||||||||
| Mid-1996 ~; | Record 22-minute flight made on 2 March 1999. | 
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Prime Manu.
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UAV Designation
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| Development | Production | Operation | Purpose | Mission payload | Launch, take-off type | Recovery, landing type | Min ground crews need | System composite | Datalink, comm frequency | Engine | Power Sources | Propulsion | Surface | Wing span | Wing area (c§³) | Length overall | Height overall | Wheel track | Wheel base | Wing aspect ratio | Fuselage max width | Weight empty | Max fuel weight | Max payload | Max T-O/launch weight | Max level speed (kt) | Cruising speed (kt) | Loiter speed (kt) | Stall speed (kt) | Service ceiling (ft) | Max rate of climb (ft/min) | Max range (nm) | Max endurance (h) | ||||
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Lockheed Martin
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MicroSTAR
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Underway | Surveillance MAV. | Chip-On-Flex Day TV Digital CMOS video camera, GPS, Gyro, Aaccelerometer, Pressure gauge, Two-axis magnetometer | Hand launched. | Belly landing. | 2.4 GHz (2000mW) | One electric motor, powered | 3 lithium batteries. | Two blade pusher prop. | 15.2 | 15 | 85 (Engine and battery: 70) | 50-300 | 0.6- 3.1 | 20 min - 1 h | |||||||||||||||||||||
| Since 1996. | 
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Arizona State Univ
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Mantis
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Underway | |||||||||||||||||||||||||||||||||||
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MLB
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Micro Dot
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Underway | |||||||||||||||||||||||||||||||||||
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Univ of Florida
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1998
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Prime Manu.
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UAV Designation
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| Development | Production | Operation | Purpose | Mission payload | Launch, take-off type | Recovery, landing type | Min ground crews need | System composite | Datalink, comm frequency | Engine | Power Sources | Propulsion | Surface | Wing span | Wing area (c§³) | Length overall | Height overall | Wheel track | Wheel base | Wing aspect ratio | Fuselage max width | Weight empty | Max fuel weight | Max payload | Max T-O/launch weight | Max level speed (kt) | Cruising speed (kt) | Loiter speed (kt) | Stall speed (kt) | Service ceiling (ft) | Max rate of climb (ft/min) | Max range (nm) | Max endurance (h) | ||||
| USA |
Univ of Notre Dame
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Virginia Polytechnic Institute and St. Univ
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Georgia Tech
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Gator
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Dragon fly
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California Polytechnic St. Univ
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Brigham Young Univ
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ASU
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HARVee
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Alcore Technologies
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SA-Epsilon2
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