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PRECISION H4WK 

# UAV SPEC F CAT ONS L ancas t e r Mk .lll R ev . 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 SouthA merica 433 M Hz Europe

EMERGENCY OVERRIDE CONTROL FREQUENCY 

# 2.4GHz POWER SOURCE 

# 6600 mAhr Lit h ium - Po lyme r Batt ery 

### CRUISE SPEED 

# 12m/s 2 7 mph 43km/h 23kn MAX TAKEOFF WEIGHT 

# 3.4kg 7.51bs

# TECHNICAL PARAMETERS

W I NGSPAN LE N GTH COMPUTATI ON 

# 1.5m 4.9ft 0.95m 3.1ft 720MHz Dual -Co re Li nux CPU W EIGHT ( N o P ayload) ENDURANC E EMBEDDE D PROCESSING 

# 2 . 4kg 5.31bs 45 min 

# 1CPU M AX PAYLOAD TYP ICAL ALTITUDE RANGE 

# 1

kg 2 .21bs 30m - 300m 98ft - 984ft SU R VEY AR EA PE R FLI GH T OPERATIO N AL SOUND I N T EN SITY AT ALT ITUDE 

# Approximately 300 Acms 100m 328 ft Altit ude 

# Approx . 

# 40dB

**--· --...........**  V i sua l ca mera , 70 % i mage overlap LINEAR FLIGHT RANGE 

# 30km 18 .6mi 16.2nmi 15 km round trip 9.3m i ro un dtri p 8 .1nm i round tri p COMMUNICATI ON S RANGE 

# 2km 1.2mi 1.07nmi PRE CISJON H4WK 

### at. O 

# l!

**~ ~** 

# TECHNICAL PARAMETERS CON. SPEED (CRUISE) W I ND/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 

# Se n so r Specif ic 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 Sena l USB El hernet D1gda l. Analog, I IC

# OPERATIONAL TEMPO

**~** 

# TAKEOFF DIST ANCE I-lAND LAUNCH 

# Om Ott run, 

# 40m 131 

# tt climb out Dista nce to 40m 131ft a lt WAT ER LAUNCH 

# 1Om 32. 8ft run , 

# 40m 131ft climb out

**~** 

# L ANDING 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 

# 1 7. 7kg
FIELD CASE DIMENSIONS 

# 45" X

# 16" X

# 14" 114.3cm X

# 40.6cm X

# 35.6cm

In tht. U< , aircraft sha ll 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 info rmat ion conduit to the operators with little manual control as the nominal vehicle operations will be fu l ly autonomous. However, the capabili ty to manually rega i n control of the vehicles and operate the system will always be available as an option and fail-safe measure. A Futaba -compat ib l e RC transm itter (here i nafter referred to as Co ntroller) is used to provide remote contro l capabil ities and manua l override for the vehicle. In thi s case, the pilot has d irect contro l of the aircraft's flight contro l surfaces. 

# r:E1 GROUND CONTROL STATION SOFTWARE Th e 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 

# (iPREC/S/ON HAWK 

# e precisionhawk.com 

# 0 @ PrecisionHawk 0008. 2015