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PRECISIONH4WK 

UAV SPEC F CAT ONS 

Lancas t e r Mk .lll Rev .4 
AIRCRAFT OVERVIEW 

TYPE 

Single Electric Motor 

Fixed Wing 

SURVEY ALTITUDE 

30m - 300m 88ft - 884ft 

FLIGHT TIME 

Up to 45 minutes 

L' en I on r .rror.r 1ental 

ondrtro and p ad w rght 

OPERATING TEMPERATURE 

14F - 140F -1 DC - 60C 

TELEMETRY DATA LINK 

815MHz North I 

South America 

433 M Hz Europe 

EMERGENCY OVERRIDE CONTROL FREQUENCY 

2.4GHz 

POWER SOURCE 

6600 mAhr 

Lithium-Polymer Battery 

CRUISE SPEED 

12m/s 2 7 mph 43km/h 23kn 

MAX TAKEOFF WEIGHT 

3.4kg 7.51bs 
TECHNICAL PARAMETERS 

W INGSPAN LENGTH COMPUTATION 

1.5m 4.9ft 0.95m 3.1ft 720MHz 

Dual-Core Linux CPU 

W EIGHT (No Payload) ENDURANCE EMBEDDED PROCESSING 

2.4kg 5.31bs 45 min 1 CPU 

MAX PAYLOAD TYPICAL ALTITUDE RANGE 

1 kg 2.21bs 30m -300m 98ft - 984ft 

SURVEY AREA PER FLIGHT OPERATIONAL SOUND INTENSITY AT ALTITUDE 

Approximately 300 Acms 

100m 328ft Altitude 

Approx. 40dB --· --........... 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 

PRECISJONH4WK at.O 

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~ ~ 
TECHNICAL PARAMETERS CON. 

SPEED (CRUISE) WIND/WEATHER/PRESSURE 

12 - 16m/s 43.2- 57.6km/h 26.8 -35.8mph 2 3 . 3 - 31 .1 kn SAMPLE RATE 

1OHz 

SPEED (MAX) 

SYSTEM DIAGNOSTIC 

25m/s 90km/h 55.9mph 48. 6kn SAMPLE RATE 

25Hz 

MAX WIND 

12.5m/s 45km/h 27.9mph 24.3kn PAYLOAD SENSOR RATE 

Sensor Specific 

TESTED TEMP RANGE 

-1 DC to 60C 14F to 140F 

L c , r I n; -1u1prr P- when 

operatmq near temperature extremes 

MAXIMUM OPERATING ALTITUDE MSL 

13,123ft 4,000m 

INTERFACING 

+ 

W1fi Senal USB Elhernet D1gdal. Analog, IIC 
OPERATIONAL TEMPO 

~ TAKEOFF DISTANCE 

I-lAND LAUNCH 

Om Ott run, 40m 131 tt climb out 

Distance to 40m 131ft alt 

WATER LAUNCH 

1Om 32. 8ft run, 40m 131ft climb out 

~ LANDING DISTANCE 

MIN APPROACY DISTANCE 

200m 656ft 

LANDING ROLLOUT 

D1stance to stop from touchdown 

Land Water Snow 

2m 6.6ft 3m B.Btt 6m 19.7ft 

PACKAGING 

TOTAL PACKED WEIGHT 

391bs 17. 7kg 

FIELD CASE DIMENSIONS 

45" X 16" X 14" 114.3cm X 40.6cm X 35.6cm 

In tht. U< , aircraft shall be rf.Jg l_,t ,, J 111 1 .. K<..1..r Jar1c. 1th 1-1 <.....FR 

part 47, and have 1dentif1callon (N Number) mark1nqs 1n 

accordance w1th 14 CFR part 45, St...bpart C. These markmqs shall 

be a large as pract1cab e. 
a GROUND CONTROL STATION 

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 thi s case, the pilot has direct control of the aircraft's flight control 

surfaces. 

r:E1 GROUND CONTROL STATION SOFTWARE 

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

PrecisionHawk Flight Planner and ArduPiane Mission Planner. 

TO PURCHASE THE PRECISIONHAWK SOLUTION 

Contact us at info@ precisionhawk.com 

Call us at 919-680-1305 

Monday-Friday 8am-5pm EST 

(i PREC/S/ONHAWK e precisionhawk.com 0 @ PrecisionHawk 0008. 2015