Aisheng ASN-1

ASN-1 UAV and its successors are Chinese micro air vehicles (MAV)s developed by Xi'an [1][2], also known as Northwestern Polytechnical University UAV Research Institute or 365th Institute[3], established in 1984.

ASN-1

ASN-1 UAV is a fixed wing MAV in conventional layout with high wing configuration and T-tail. Propulsion is provided by a two-blade propeller driven piston engine mounted on the wing. Specification:[4]

  • Wingspan (m): 3
  • Length (m): 1.8
  • Max weight (kg): 6.5
  • Max speed (km/h): 90
  • Ceiling (km): 0.5
  • Minimum operating altitude (m): 50
  • Remote control radius (km): 10
  • Endurance (hr): 2
  • Fuel: gasoline
  • Launch: by hand

ASN-15

ASN-15 is a development of ASN-1 MAV and share the same configuration, and externally, they look almost identical to each other. Specification:[5]

  • Speed (km/h): 80
  • Normal operating altitude (km): 0.5
  • Ceiling (km): 3
  • Endurance (h): 1
  • Remote control radius (km): 10
  • Weight (kg): 6
  • Launch: by hand
  • Recovery: glide or parachute

ASN-217

ASN-217 is a further development of ASN-15, and it is a fixed wing MAV in conventional layout with high wing configuration and T-tail. ASN-217 share the identical layout of ASN-1 and ASN-15, and as with these earlier members of this series, ASN-217 is also electrically powered. Specification:[6]

  • Take-off weight (kg): 5.5
  • Payload (kg); 1.5
  • Ceiling (km): 4
  • Max speed (km/hr): 120
  • Cruising speed (km/hr): 40 – 70
  • Endurance (hr): 1.5
  • Remote control radius (km): 20
  • Wingspan (m): 2.7
  • Length (m): 1.7
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See also

  • List of unmanned aerial vehicles of the People's Republic of China

References


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