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# UAV SPI 

# IFI ATIONS

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# MIIAd1AU IlVdAIV

# 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.~ ~ 

# 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.

# ~

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