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Pointer
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Background: AeroVironment's FQM-151A/Pointer, a hand-launched UAV, first flew in 1986 and entered operations with the US Marine Corps in June 1988. Its manufacturer focuses on environmentally friendly energy conversion projects and has built over 100 Pointers. Besides the Marine Corps, who deployed three Pointer systems in the 1991 Gulf War, its customers include the US Army, Oregon National Guard, and Special Operations Command.

Characteristics:

Length, ft 6 Wing Span, ft 8
Gross Weight, lbs 9.1 Payload Weight, lbs 2.0
Fuel Capacity, lbs 2.2 Fuel Type NiCd or Li batteries
Engine Make Astro 15 electric Power, hp 300 w
Structure Kevlar  
Guidance   Navigation Motorola GPS
Data Link(s) 4105-4115/72-7400 up
1730-1820 dn
Data Rate(s)  

Performance:

Endurance, hrs 1 (NiCd)/2.2 (Li) Radius, nm 1 (LOS)/3 (link)
Max Speed, kts 43 Stall Speed, kts 16
Altitude, ft 3,000  
Takeoff Means Hand-launched  
Navigation Modes Preprogrammed (points)/
autonomous/direct control
 
Landing Means Stall  

Sensor(s): EO (day TV), IR (Microcam), various atmospheric sampling payloads