AUSTRALIA
  Prime Manu.
  UAV Designation
Production status  
Operational status 
Power plants
Dimensions (m) 
  Wieghts (kg)  
        Performance      
 
Comments
 Development
Production
Operation
 Purpose
Mission payload
Launch, take-off type
Recovery, landing type
Min ground crews need
System composite
Datalink, comm frequency
Engine
Propulsion
Wing span
Wing area (§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)
Range (nm)
Max Endurance (h)
Tempest
Vindicator
Complete
 
 
 
 
 
 
 
 
Piston
 
 
 
 
 
 
 
 
1,050
 
 
23.1
200
 
 
 
 
25,000
 
110
20.0
 
                                                                 
Aerosonde Robotic Aircraft
Aerosonde Mark ¥±
Complete Completed Deployed Weather Research Sonde         UHF/VHF/SAT com Piston 4 stroke                       9.5 28 (14~15Kg) fuel: (AVGAS) 7liter 5         20,000   3000km with Sat Comm 36.0  
                                                                 
KEOP-2001 (Korea Enhance Observation Period 2001) KMA(METRI)-Aerosonde-Gongbo Engineering                                                              
                                                                 
                                                                 
                                                        ¡Ø Typhoon Hunter 2001        
Aerosonde Mark ¥²
Complete Underway                 Piston 4stroke injection engine                                   20,000   3000km with Sat Comm 45 UHF/VHF/SAT com AGRF Weather Research