Ababil-T Iranian Loitering Munition Unmanned Aerial Vehicle (UAV)

type

"WEG"

version

1

images

"Ababil_II.jpg"

categories

"WEG"

"Theater Missiles"

"Cruise Missile"

"Anti-ship CM"

"Tier2"

tiers

false

true

false

sections

name

"System Name"

properties

name	"Producing Country"
value	"Iran"

name	"Alternative Designation"
value	"Ababil-CH, Swallow, Mirsad-1, Qasef-1"

name	"Date of Introduction"
value	"1992"

name	"Proliferation Countries"
value	"3"

name	"Crew"
value	"2"

name	"Ground Crew"
value	"1"

name	"Propulsion"
value	"Twin cylinder piston engine fitted with a two blade pusher prop"

name	"Fuel Capacity (l)"
value	"16"

name	"Motor (hp)"
value	"12"

name	"Length (m)"
value	"2.8"

name	"Height (m)"
value	".25"

name	"Gross Takeoff Weight (kg)"
value	"80"

name	"Max Speed (km/h)"
value	"275"

name	"Max Ceiling (m)"
value	"4250"

name	"Operational Altitude (m)"
value	"3000"

name	"Endurance (min)"
value	"105"

name	"Range (km)"
value	"100"

name	"Launch Method"
value	"Rail Catapult, Rail Rocket"

name	"GNSS Enabled"
value	"Yes"

name	"Recovery Method"
value	"Parachute"

name	"Automatic Pilot Controls"
value	"Yes"

name	"Operating Frequency (GHz)"
value	".9"

name	"Power"
value	"INA"

name	"Controller Endurance"
value	"INA"

name	"Gimbal Stabilized Camera"
value	"Yes"

name	"Camera Resolution (MP)"
value	"INA"

name	"Camera Range (m)"
value	"400 est."

name	"Warhead Weight (kg)"
value	"17"

notes

"The Ababil-II family of UAVs is produced by Iran’s Aircraft Manufacturing Industrial Company (Hesa). The Ababil II is distinguished by its front stabilizing canards and dual tail fins on the back Wing."