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Tunisia |
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Prime Manu.
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UAV Designation
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Production status
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Operational status
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Power plants
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Dimensions (m)
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Wieghts (kg)
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Performance
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Comments
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Development
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Production
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Operation
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Purpose
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Mission payload
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Launch, take-off type
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Recovery, landing type
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Min ground crews need
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System composite
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Datalink, comm frequency
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Engine
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Propulsion
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Wing span
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Wing area (§³)
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Length overall
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Height overall
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Wheel track
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Wheel base
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Wing aspect ratio
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Fuselage max width
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Weight empty
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Max fuel weight
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Max Payload
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Max T-O/launch weight
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Max level speed (kt)
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Cruising speed (kt)
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Loiter speed (kt)
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Stall speed (kt)
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Service Ceiling (ft)
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Max rate of climb (ft/min)
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Range (nm)
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Max Endurance (h)
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TAT (Tunisia Aero Tech- nologies sarl) e-mail |
Nasnas Mk„° |
Underway |
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Reconnaissance and multipurpose prototype UAV |
High-resolution film camera, TV camera or FLIR. |
Wheeled take-off standard and catapult launch optional. |
Wheeled landing, parachute optional. |
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One 10 hp modified Canadian chain-saw engine in prototype; in 1998 25 hp flat-twin substituted.; production version has 22 hp flat-twin two-stroke with electronic ignition.. |
Two-blade pusher prop. |
3.80 |
2.05 |
2.80 |
1.30 |
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43 |
14 liter wing tank and 20 liter fuselage tank; combined 48 liters.; wingtip tanks containing futher 16 liters. |
25 |
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70 |
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25 |
16,400 |
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14.0 |
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First flight in August 1998. |
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Super Nasnas |
Underway |
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HALE virsion. |
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6.90 |
3.80 |
4.70 |
1.30 |
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158 |
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270 |
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75 |
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17,060 |
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16.0 |
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