Test Drive | Page 4

MEDIUM ALTITUDE LONG ENDURANCE 
ISR UNMANNED  AERIAL SYSTEM
DIMENSIONS
Span
Length
Height

15.600 m
14.408 m
3.980 m

[51.18 ft]
[47.27 ft]
[13.05 ft]

AREAS
Wing
Horizontal Tail
Vertical Tail
Forward Wing (Exposed)

18.00 m2
3.834 m2
4.731 m2
1.300 m2

WEIGHTS
Max TakeOff Weight MTOW

6,146 Kg [13,550 lbs.]

[193.75 ft2]
[41.27 ft2]
[50.92 ft2]
[13.99 ft2]

POWERPLANT  
2 × Pratt & Whitney Canada PT6A-66B 850 SHP
(ISA, sea level)
Hartzell five blade low noise propellers counter rotating.
PERFORMANCE
Maximum speed: 
Cruise speed:  
Loiter speed:     
Max Range:        
Max Endurance (500 lbs payload):
Endurance (500 lbs payload)
@ 1,500 km from takeoff & landing base
Service ceiling:
Mission system

395 KTAS
320 KTAS
135 KTAS
4,400 NM
16 hours
10.5 hours
45,000 ft

Selex ES SkyISTAR® with:
FLIR EO/IR StarSafire 380HD
Seaspray 7300 E Radar

Piaggio Aerospace
P.1HH HammerHead
UAS
Capable to perform
ISR – COMINT - ELINT – SIGINT missions   
All weather operation
Automatic takeoff & landing 
Compliant with STANAG-USAR 4671         
Full redundancy – Safety requirements
Cat. Event Prob. 10-6 FH, SW Critical
functions DO178B level B
System is ground/sea/air transportable
(removable wings)
24 hrs deployment capability