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UAV SPI IFI ATIONS 

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TFCHNICAL PARAMFTFRS 

WINGSPAN LENGTH 

1,5m 4,9fit 0,95m 3,1 ft 

WEIGHT (No Payload) ENDURANCE 

2,4kg 5,3ibs 45 min 

MAX PAYLOAD 

1 kg 2,2ibs 

SURVEY AREA PER FLIGHT 

Approximately 300 Acres 

100m 328ft Altitude 

Visual camera, 70% image overlap 

LINEAR FLIGHT RANGE 

30km 18,6mi 16,2nmi 

15km roundtrip 9.3mi roundtrip 8.1nmi roundtrip 

COMMUNICATIONS RANGE 

2km 1, 2mi 1, 07nmi 

COMPUTATION 

720MHz 

Dual-Core Linux CPU 

EMBEDDED PROCESSING 

1 CPU 

TYPICAL ALTITUDE RANGE 

30m - 300m 98ft - 984ft 

OPERATIONAL SOUND INTENSITY AT ALTITUDE 

Approx, 40dB 

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PAYLOAD SENSOR RATE 

Sensor SpecifiC 

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TFCHNICAL PARAMFTFRS 

SPEED (CRUISE) 

12 -16m/s 43,2 - 57 ,6km/h 26,8 - 35,8mph 23,3 - 31,1 kn 

SPEED (MAX) 

25m/s 90km/h 55,9mph 48,6kn 

WI N D/WEATH ER/PRESSURE 

SAMPLE RATE 

10HZ 

SYSTEM DIAGNOSTIC 

SAMPLE RATE 

2SHz 

MAX WIND 

12,5m/s 45km/h 27,9mph 24,3kn 

TESTED TEMP RANGE 

-10C to 60C 14F to 140F 

*Do not prolong equipment exposure when 

operating near temperature extremes 

MAXIMUM OPERATING ALTITUDE MSL 

13,123fit 4, OOOm 

INTERFACING 

^ m T 'tf '1' 

Wifi Serial USB Ethernet Digital, Analog, IIC 
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OPFRATIONAL TFMPO PACKAGING 

HAND LAUNCH 

Om Ott run, 40m 131 ft climb out 

Distance to 40m 131ft alt 

WATER LAUNCH 

10m 32,8ft run, 40m 131 ft climb out 

y- LANDING DISTANCE 

MIN APPROACH DISTANCE 

200m 656ft 

LANDING ROLLOUT 

Distance to stop from touchdown 

Land Water Snow 

2m 6,6it 3m 9,8tt 6m 19,7it 

TOTAL PACKED WEIGHT 

391bs 17,7kg 

FIELD CASE DIMENSIONS 

45" x 16" x 14" 114,3cm x 40,6cm x 35,6cm 

*In the U-A, aircraft shall be r-:y,-[ered in a` , ; dancu 4 CFR 

part 47, and have identification (N-Number) markings in 

accordance with 14 CFR part 45, Subpart C. These markings shall 

be as large as practicable. 
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GROUND CONTROLSTATION 

The ground control station (hereinafter referred to as GCS) will include a single 

computer in communications contact with the vehicle system. This station will 

primarily act as an information conduit to the operators with little manual 

control as the nominal vehicle operations will be fully autonomous. However, 

the capability to manually regain control of the vehicles and operate the 

system will always be available as an option and fail -safe measure. 

A Futaba- compatible RC transmitter (hereinafter referred to as Controller) is 

used to provide remote control capabilities and manual override for the 

vehicle. In this case, the pilot has direct control of the aircraft's flight control 

surfaces. 

~ GROUND CONTROLSTATION SOFTWARL 

The Aircraft Ground Station Software (hereinafter referred to as GSS) is the 

PrecisionHawk Flight Planner and ArduPlane Mission Planner. 

TO PURCHASLTHL PRLCISIONHAWK SOLUTI0N _ 

Contact us at info@ precisionhawk.com 

Call us at 919 -680 -1305 

Monday - Friday 8am - 5pm EST 

PREC/S/ONH4WK ® precisionhawk.com 0 @ PrecisionHawk