Surveying And Mapping, LLC

4801 Southwest Parkway, Building Two, Suite 100, Austin, TX 78735

Ofc 512.447.0575 Fax 512.326.3029

info@sam.biz www.sam.biz TX Firm # 10064300

August 2 5 , 2015

U. S. Department of Transportation

Docket Management System

1200 New Jersey Ave., SE

Washington, DC 20590

RE: Request to Amend Exemption Number 11393 (Granted 20 April 2015) issued

pursuant to Section 333 of the FAA Reform Act and Part 11 of the Federal Aviation

Regulations in Regulatory Docket No. FAA

- 2014

- 0353

- 0001

Dear Sir or Madam:

Pursuant to Section 333 of the FAA Modernization and Reform Act of 2012, Pub. L. No. 112

- 95,

126 Stat. 11 (amending 49 U.S.C.) (hereinafter, the “ Reform Act ”) and 14 C.F.R. Part 11,

Surveying And Mapping, LLC (“ SAM ” or “ Applicant ”) , developer and operator of small

unmanned aircraft systems (singularly a “ sUAS ” or cumulatively “ sUASs ”) equipped to conduct

professional aerial land surveying and geospatial services , hereby applies for a petition to amend

Exemption Number 11393, granted April 20, 2015 (the “ Exemption ” ) , to allow commercial

operation of two (2) additional sUAS, provided such operations are conducted within and under

the conditions outlined by the grant of the Exemption.

As SAM is only requesting to add aircraft to the Exemption

, it is our position this amendment does

not qualif y as precedent

- setting, per guidance locate d at: http://aes.faa.gov/Petition/faq5a.html

. Therefore, t he Applicant respectfully submits that good cause exists such that notice does not need

to be published in the Federal Register for the requested amendment

.

Currently, per paragraph 1 of the section of the E xemption nam ed “Conditions and Limitations,”

SAM’s exemption is limited to operations using the Allied Drones HornetCam, and proposed

operations of any other aircraft require a petitio n to amend the E xemption.

The name and address of the A pplicant is:

Surveying And Mapping, LLC

Attention: Pat Smith

4801 Southwest Parkway

Bldg. Two, Suite 100

Austin, TX 78735

Telephone: (512) 685

- 3542

Email: psmith@sam.bizU. S. Department of Transportation

Docket Management System

August 25, 2015

2 | Page The Applicant hereby requests to amend the Exemption , and the issuance of an FAA Form 7711

- 1 UAS COA Attachment, to allo w the use of the following two (2) sUAS:

1. SenseFly eXom ; and

2. Aeryon Skyranger

(Aircraft numbered 1 and 2 above, collective ly the “ Amendment Aircraft ”)

.

In parallel to the Exemption , the Amend ment A ircraft will be used for commercial aerial data

collection by Applicant. Aircraft technical data and checklists for the Amend ment Aircraft are attached to this p etition, labeled Annex A ( SenseFly eXom D atasheet ) and Annex B ( Aeryon

Skyranger D atasheet) , respectively

. Previously granted exemptions to other applicants , including

Exemption No. 12106, allowed for the use of the Amendment Aircraft. For commercial

purposes, and it is Applicant’s position, this petition to amend the Exemption is similar in

material respects to the aforementioned granted exemption. In accor dance with the conditions

and limitations granted to SAM under the Exemption , the A pplicant respectfully requests

exemption from the following while operating the Amendment Aircraft:

14 CFR §§ 61.23(a) and (c), 61.101(e)(4) and (5), 61.113(a), 61.315(a), 91.7(a), 91.119(c),

91.121, 91.151(a)(1), 91.405(a), 91.407(a)(1), 91.409(a)( 1 ) and (2), and 91.417(a) and (b), to the

exte n t n e cessary to al low the petitioner to operate a UAS to perform a e rial data collection.

In accordance with the section of the Exemption known as “Conditions and Limitations,” SAM

hereby requests to operate the Amendment Aircraft while adhering to the conditions and

limitations listed below:

1. Operations authorized by this amendment to the Exemption are li m ited to the SenseFly

eXom and the Aeryon Skyra nger

, when weighing less than 55 pounds including payload.

Proposed operations o f any other a i rc r a f t will r equire a new petition or a petition to a m end

this exe mption.

2. Operations for the purpose of closed

- set m otion picture and television fil m ing are not

per m itt e d.

3. The UA m a y not be operated at a s p eed excee d ing 87 knots (100 m iles per hour). T h e

exe m ption holder m ay use either groundspeed or calibrated airspeed to deter m ine

co mpliance with the 87 knot speed restrict i on. In no case will the UA be operated at

airspeeds greater than t h e m ax i m u m UA operating airspeed recommended by the aircraft

m anufacturer.

4. The UA m u st be operated at an altitude of no m o re than 400 f eet above ground level

(AGL). Altitude m ust be reported in f eet AGL.

5. The UA m u st be operated within visual line of sight (VLOS) of the PIC at all ti m es. This

req u ir e s the PIC to be able to u s e hu m an vision unaided by any device other thanU. S. Department of Transportation

Docket Management System

August 25, 2015

3 | Page correcti v e lenses, as specified on the PIC’s FAA

- issued air m an m edical certifi c ate o r U.S.

driver ’ s li c ense.

6. All oper a ti o ns m ust utilize a vis u al o bserver (VO). The UA must be op e rated within the

visual line of sight (VLOS) of the PIC and VO at all ti m es. The VO m ay be used to

satisfy the VLOS require m ent as long as the P IC always maintains VLOS capability. T he

VO and PIC m ust be able to communicate verbally at all ti m es; ele c tronic messaging o r

texting is not per m itted d uring f lig h t operations. The PIC m u st be designated before the

flight and cannot transfer his or her designation for the duration of the flight. T he PIC

m ust ensure t h at the VO can perform the duties required of the VO.

7. This exe mption and all docu m ents needed to operate the UAS and conduct its operations

in accorda n ce with the conditions a n d li m itations stated in t h is grant of exe mption, are

hereinafter referred to as the “ operating docu m ents. ” The operating docu m ents must be

accessible during UAS operations and made available to the Ad m i nistrator upon request.

If a discrepancy exists between the conditions and li m itations in this e x e mption and the

procedu r es outli n ed in the oper a ting docu m ents, the conditions and li m itations herein t a ke

precedence and must be followed. Otherwise, the oper a tor must f ollow the procedures as

outlined in its operating docu m ents. The operator m ay update or rev i se its operating

docu m ents. It is the operator’s responsibility to track such revisions and present updated

and revised docu m ents to the Ad m i nistrator or any l a w enforce m ent official upon request.

The operator m u st also present updated and revis e d docu m ents if it petitions for extension

or a m end m e nt to this grant of exe m p t ion. If the operator deter m ines that any update or

revision would affect the basis upon which the F AA granted this exe mption, then the

operator m u st petition for an a m end m ent to its grant of exemption. The FAA’s UAS

Integration Office (AFS

- 80) m ay be contact e d if questions arise regarding updates or

revisions to the operating docu m ents.

8. Any UAS t hat has undergone m aintenance or alterations that affect the UAS operation or

flight characteristics, e.g. replace m ent of a f light critical co m ponent, m u s t undergo a

functional test flight prior to conducting further operations under this exe mption.

Functional test flights may only be conducted by a PIC with a VO and must re m ain at

least 500 feet from o t her people. The functional t e st flight m ust be conducted in such a

m a nner so as to not po s e an undue hazard to persons and propert y

.

9. The operator is responsible for m aintaining and inspecting the UAS to ensure that it is in a

condition for safe operation.

10. Prior to each flight, the P IC m ust conduct a pre

- flight ins p ection and deter m ine the UAS

is in a condition for safe flight. T h e pre

- fli g ht inspecti o n m ust acc o unt for all potential

discrepancies, e.g. inoperable co mponents, ite m s, or equip m ent. If the inspection reveals a

co n dition that affects the safe operation of the UAS, the aircraft is prohibited from

operati n g until the n ecess a ry m a intena n ce h a s been perf o r m ed and the UAS is found to beU. S. Department of Transportation

Docket Management System

August 25, 2015

4 | Page in a condition for safe flight.

11. The operat o r m ust f ollow the UAS m anufacturer’s m aintenance, overhaul, replace m ent,

inspection, and life li m i t req u ire m ents for the aircraft and aircraft co mponents.

12. Each UAS operated un d er t h is exe mption m ust co mply with all m anu f acturer sa fe ty

bull e tins.

13. Under this grant of exemption, a PIC must hold either an airline transport, commercial,

priv a t e, r e c r eatio n al, or sport p i lot certificate. T he PIC m ust also hold a curre n t FAA

air m an m edical certificate or a valid U.S. driver’s license issued by a state, the District of

Colo m bia, Puerto Rico, a territory, a possession, or the Federal govern m ent. The PIC

must also meet the flight review require m ents specified in 14 CFR § 61.56 in an aircraft in

which the P I C is rated on his or her pilot certificate.

14. The operator m ay not per m it any PIC to operate unless the PIC de m onstrates the ability to

sa f ely ope r ate the UAS in a m a nner co n siste n t with how the UAS will be operated under

this exemption, including evasive and e m ergency m aneuvers and m aintaining appropriate

distances from persons, vessels, vehicles and structures. PIC qualification flight hours

and currency m ust be logged in a manner consistent with 14 CFR § 61.51(b). Flights for

the purposes of training the operator’s P ICs and VOs (training, proficiency, and

experience

- building) and deter m i ning the PI C ’s ability to sa f ely oper a te the UAS in a

m anner consistent w ith how the UAS will be operated under t h is exe m ption are per m itted

under the ter m s of this exe m ption. However, training operations m ay only be conducted

du r ing dedicated training sessions. During training, proficiency, and experience

- building

flights, a l l persons not essential for flight operations are considered nonparti c ipants, and

the PIC m ust operate the UA with appro p riate distance from nonparticipa n t s in

accorda n ce with 14 CFR § 91.119.

15. UAS operations m ay not be conducted during night, as defined in 14 CFR § 1.1. All

operations must be conducted under visual m eteorological condit i ons (VMC). Flights

under special visual flight rul e s (SVFR) are not authorized.

16. The UA m a y not operate within 5 nautical m iles of an airport refere n ce p oint (ARP) a s

denoted in the current F AA Airport/Faci l ity Directory (AFD) or for airports not denoted

with an ARP, the center of the a i rport sy m bol as denoted on the current FAA

- published

aeronautical chart, unless a let t er of a g ree m ent with that airp or t’s m anage m ent is obt a i ned

or otherwise per m itted b y a COA issued to the e xe m ption holder. The letter of agree m ent

with the a i rport m anage m ent must be m ade available to the Ad m i nistrator or any law

enforce m ent official upon request.

17. The UA m a y not be operated less than 500 feet below or less than 2,000 feet horizontally

from a cloud or when visibility is less than 3 statute m iles from the PIC.U. S. Department of Transportation

Docket Management System

August 25, 2015

5 | Page 18. If the UAS loses com m unications or loses i t s GPS signal, the UA m ust return to a pre

deter m ined location wit h in the p ri v ate or controlled

- access property.

19. The PIC m u st abort the f light in the event of unpredicted obstacles or e m ergencies.

20. The PIC is prohibited from beginning a flight unless (considering wind and forecast

weather conditions) there is enough available power for the UA to conduct the intended

operation and to operate after that for at least five minutes or with the reserve power

recommended by the m anufacturer if greater.

21. Air Traffic Organizati o n (ATO) Certificate of Waiver or A utho r ization (COA). All

operations shall be conducted in accord a nce with an ATO

- issued COA. The exe mption

holder m ay apply for a new or a m ended COA if it intends to conduct operations that

cannot be conducted under the ter m s of the attached COA.

22. All aircraft operated in accor d a n ce with this exemption m ust be identified by serial

nu m ber, registered in accordance with 14 CFR p a rt 47, and have identification (N

Nu m ber) m arkings in accordance with 14 CFR p a rt 45, Subpart C. Markings m ust be as

lar g e as p ractica b le.

23. Docu m ents used by the operator to ensure t h e safe operation and flight of the UAS and

any docu m e nts required under 14 CFR §§ 91.9 and 91.203 m u st be available to the PIC at

the G round Control Station of the UAS any ti m e the aircraft is operating. These

docu m ents must be m ade available to the Ad m i nistrat o r or a n y law enforcement official

upon request.

24. The UA m u st re m ain clear and give w a y to all m anned aviation operations and acti v ities

a t all ti m es.

25. The UAS may not be operated by the PIC from any m oving device or vehicle.

26. All Flight operations must be conducted at least 500 feet from all nonparticipating

persons, vessels, vehicles, and structures unless:

a. Barriers or structures are present that sufficiently p r otect nonparticipating persons

from the UA and/or de b ris in the eve n t of an acci d ent. The operator m ust ensure that

nonparticipating persons re m ain under such protection. If a situation arises where

nonparticipating persons leave such protection and are within 500 feet of the UA,

flight operatio n s m ust cease im m ediately in a m anner ensuring the safety of

nonparticipating persons; andU. S. Department of Transportation

Docket Management System

August 25, 2015

6 | Page b. The owner/controller of any vessels, vehicles or struc t ures has granted per m ission

for operating closer to those objects and the PIC has m ade a safety assess m ent of the

risk of operating closer to those objects and deter m ined that it does not present an

u ndue hazard.

The PIC, VO, operator trainees or e s sential pers o ns are not c o nsidered

nonparticipating persons under this exe m ption.

27. All operati o ns shall b e conducted o v er pri v ate o r contr o lle d

- access pro p erty with

per m ission from the property owner/controller or authorized representative. Per m ission

from property owner/co n t roller o r authorized rep r esent a tive w ill b e obtained for each

flight to be conducted.

28. Any incident, accident, or flight operation that tr a nsgress e s t h e later a l or v ertical

boundaries of the operational area as defined by the applicable COA must be reported to

the FAA ' s UAS Integration Office (AFS

- 80) within 24 hours. Accidents m ust be reported

to the National Transportation Safety Board (NTSB) per instructions contained on the

NTSB Web site: w ww.ntsb.gov

.

Unless otherwise specified in this grant of exemption, the UAS, the UAS PIC, and the UAS

operations must co m p l y with all applicable parts of 14 CFR including, but not li m ited to, parts

45, 47, 61, and 91.

Summary

Approval of this amendment to the granted Exemption and the issuance of an FAA Form 7711

- 1

UAS COA Attachment, allowing the operation of the Amendment A ircraft listed in this petition

will provide an equivalent level of safety supporting the amendment requ ested herein. The

Amendment Aircraft possess even more enhanced safety features than the Allied Drones

HornetCam which was previously approved for use in the Exemption, and when operated within

the conditions and limitations outlined in the Exemption

, are far safer than conventional

operations conducted with manned aircraft used for aerial data acquisition.U. S. Deparhnent of Transportation

Docket Management System

August 25,2015

Please let me know 

### if you have any questions concerning this request for an amendment to the

Exemption

Very truly yours,

Patick A. Smith, RPLS

Associate

Surveying And Mapping, LLC (SAM)

4801 Southwest Parkway

Parkway Two, Suite 100

Austin, TX78735

Direct 512.685.3542



### Email: osmithØsam.biz

Attachments:

Annex 

### A (Sensefly eXom Datasheet)

Annex B (Aeryon Skyranger Datasheet)



### TlPageAnnex A

Sensefly eXom Datasheet

## The intelligent mapping

& inspection drone Technical specifications

Source

Number

Video

Horizontal field of view

Availability Software application

Mission planning

Flying

After your flight

Software application

Processing

rayCloud Editor

Mosaic Editor

Output results Material

Function

Navigation lights

Anti-collision lights

Avoidance procedure

Warning signals

Cruise control

Distance lock

Obstacle avoidance

Automated failsafe behaviours

Operator triggered

Type

Manual RC control Sensor

Number

Range

Feedback 

### Situational awareness & assistance Ground station software

Image processing Operational safety

Multidirectional video feed

Shrouding

Signalisation lights

Ground proximity detection

Flight assistance features (Interactive mode)

Safety procedures

Autopilot fallback Object & range detection Navcams (visual sensor)

5

VGA (640 x 480 pixels)

100 degrees

One navcam at a time senseFly eMotion X (supplied)

Intuitive 3D user interface

Click and drag to set mission blocks

Automatic 3D flight planning

Edit mission plans during flight

Automated system checks

Automated take-off & landing

Real-time flight status

Main camera video feed integration

Thermal video feed integration

Navcam video feed integration

Fully automatic flight

Interactive ScreenFly

Manual flight (with assistance

functions)

In-flight switch between flight modes

Black-box recording of all flight &

mission parameters

Project & data management

Seamless interface to Postflight

Terra 3D

DNG to JPEG conversion

Postflight Terra 3D (supplied)

Rapid Check processing

Quality Report

Automatic Aerial Triangulation (AAT)

and Bundle Block Adjustment (BBA)

Automatic point cloud classification

and DTM extraction

Point cloud filtering and smoothing

Automatic brightness and colour

correction

Point cloud viewing & editing

Polyline, surface & stockpile

measurement

Digitisation tools/vector object

editing

Fly-through animation

Seamline editing

Planar/ortho projection selection

Mosaic colour/brightness editing

2D and 3D (orthoimage, point

cloud, vector data, etc.)

Optimised camera position,

external orientation and internal

parameters, undistorted images Carbon fibre

Defines propeller rotation area

Protects from damage at low speed

2 green on the right, 2 red on the left

1 top strobe, 1 bottom strobe

Automatic stop (can be deactivated)

Audio & visual

Maintains (low) constant speed in a

given direction

Keeps distance to frontal objects

3 - 5 m (9.8 – 16 ft)

Depending on flight phase

Geofencing, return home,

emergency stop, emergency landing

Hold position, return home, go land,

land now, emergency motor cut-off

Independent low-level autopilot

(backup for main autopilot)

Independent RC controller

(take manual control at any time) Ultrasonic

5

Up to 6 m (20 ft)

Audio and visual object warningType

Dimensions (incl. shrouding)

Engines

Propellers

Take-off weight

Flight time (full system)

Max. climb rate

Max. airspeed

Wind resistance

Autopilot & control

Materials

Operating temperature

Type

Frequency

Data transmitted

Range

Technology

Type

Power level display

Charging time Type

Frequency

Range 

### Flight system

Wireless communication

System power Main communication link

RC (Remote control) V-shaped quadcopter

56 x 80 x 17 cm (22 x 32 x 7 in)

4 electric brushless motors

4

1.7 kg (3.7 lb) incl. battery, payload &

shrouding

Up to 22 min

7 m/s (15 mph)

Automatic flight: 8 m/s (18 mph)

Manual flight:12 m/s (27 mph)

Automatic: up to 8 m/s (18 mph)

Manual: up to 10 m/s (22 mph)

IMU, magnetometer, barometer

& GPS

Composite body, moulded carbon

fibre arms and legs, precisionmolded magnesium frame,

precision-molded injected plastic

-10 to 40o C (14o-104o F)

Digital, dual omnidirectional

antennas, dual band, encrypted

2.4 GHz & 5 GHz ISM bands

(country dependent)

Commands, main camera stream,

navcam stream, sensor data, etc.

Up to 2 km (1.2 mi)

Smart battery

LiPo, 3 cell, 8500 mAh

LED display on battery, on-screen

information

1 - 1.5 h Digital

2.4 GHz

Up to 800 m (0.5 mi) Control interface

Mission planning

Types of mission blocks

In-flight mission changes Types

Availability

Type

Quad-core processor

Dual-core processor

Single-core processor

Single-core processor Primary control interface

Flight assistance

(depending on the flight phase)

Primary control interface 

### Flight modes

On-board computing Automatic

Interactive ScreenFly

Manual (RC) Mouse, keyboard or touchscreen

Drag-and-drop mission blocks

Horizontal mapping

Around point of interest

User-defined route

Yes: manual waypoint changes and

updates possible at any time Automatic

Interactive ScreenFly

Manual (RC)

Switch between modes at any time

4 on-board CPUs

Principal autopilot & artificial

intelligence

Video co-processing

Low-level autopilot (safety fallback)

and motor control

Communication link management

The information contained in this brochure is for promotional purposes only and

does not constitute an offer, warranty or contract. Screen-based actions & USB joypad

Cruise control

Distance lock

Obstacle avoidance

RC (remote control) Still images

Video

Horizontal field of view

Digital zoom

Number

Positions

Video

Horizontal field of view

Availability

Operational use Still images/video

Horizontal field of view

Edge enhancement

Video

Video live streaming range

Horizontal field of view

Headlamp

Flash 

### Integrated payloads

Main camera

Thermal camera

Head navcam (visual sensor)

Lights

38 MP, mechanical shutter

DNG (RAW image with correction

metadata)

Ground sampling distance (GSD):

- 1 mm/pixel at 6 m

- 1 cm/pixel at 60 m

Recorded on board

Geo-referenced (position &

orientation)

HD (1280 x 720 pixels)

Recorded on board or streamed

63 degrees

6x

4 navcams

Left, right, rear, bottom

VGA (640 x 480 pixels)

100 degrees

One navcam at a time

Side views (w/o turning main

camera) & parallel flight along

objects

Back-up safely & control in

tight environments

Landing & ground proximity Thermal (80 x 60 pixels) overlaid on

main camera stream

50 degrees

Yes

VGA (640 x 480 pixels)

Up to 2 km (1.24 miles)

100 degrees

Yes, used for video

Yes (not active upon release) TripleView head

Additional navcams (visual sensors)

For eXom updates

subscribe to our newsletter at

www.sensefly.comAnnex B

Aeryon Skyranger DatasheetField-tested and battle-proven, Aeryon small UAS set the

standard for immediate aerial intelligence gathering by ANYONE

, ANYWHERE , at ANYTIME :

Intuitive touchscreen interface and advanced features, minimal user training

Single operator transport and deployment, no launch or recovery equipment

Reliable flight performance even in the most demanding weather conditions,

when other systems cannot fly

The Aeryon SkyRanger TM introduces a new airframe and integrated system

design to the Aeryon sUAS platform, based on thousands of hours of flight

time and successful customer exercises and missions around the world.

Designed to military and government specifications, SkyRanger TM extends

industry-leading performance and system capabilities.

Intuitive interface and autonomous

capabilities – no joysticks required

Advanced optics and networking – smart

imagery and seamless integration Pre-assembled deployment –

airborne in seconds

Rugged, reliable and capable –

dependable in extreme environments Point-and-click touchscreen navigation

and camera control

Dynamic flight plans including Follow-Me TM

protection and AutoGrid TM mapping modes

Stabilized, simultaneously-streaming

dual EO/IR high resolution cameras

-	 EO: 1080p24 HD H.264 video,

15MP still images

-	 IR: 640x480 H.264 video and still images,

white-hot and black-hot modes

Low-latency all-digital network

– 256bit AES

encrypted streaming video to multiple devices,

embedded geotags and metadata

Beyond line-of-sight range

– 1.9 mi (3 km) integrated capability,

extensible beyond 3.1 mi (5 km) Folding design protects payload &

includes battery for powered standby

Payload, battery, arms and legs are

easily replaced in the field without tools

Up to 50-minute endurance with payload,

continuous operation model

High wind tolerance

- 40 mph (65 kph) sustained

- 55 mph (90 kph) gusts

Ruggedized and weather-sealed

Environmental temperature range

-22 o F to 122 o F (-30 o C to 50 o C)The Aeryon sUAS platform brings secure, real-time and simultaneous tactical situational

awareness to ground forces and remote command. Advanced autonomous capabilities

and simple touchscreen controls require minimal training for soldier, squad, or

platoon-level deployment.

Unlike fixed-wing systems, the Aeryon SkyRanger TM is a Vertical Take-Off and Landing (VTOL)

sUAS

– ideal for providing continuous eyes-on-target for situational awareness, operations

in confined environments, and low-risk launch and retrieval without peripheral equipment.

SkyRanger TM is ideally suited for both land and maritime military use including covert ISR,

convoy and compound security, and ship boarding operations.

Immediate deployment, small size, quiet operation and specialized imaging payloads

make SkyRanger TM the ideal platform for a wide range of missions in any conditions, including:

Tactical situational awareness & targeting

Perimeter & convoy security

Covert Intelligence, Surveillance

and Reconnaissance (ISR)

Copyright © 2015 Aeryon Labs Inc.

- All rights reserved. Aeryon, Aeryon Labs and SkyRanger are trademarks of Aeryon Labs Inc.Printed in Canada TECHNICAL SPECIFICATIONS:

ENDURANCE:

• Up to 50-minute flight time (with payload)

WIND TOLERANCE:

• 40 mph (65 kph) sustained

• 55 mph (90 kph) gusts

ENVIRONMENTAL TEMPERATURE RANGE:

• -22 o F to –122 o F (-30 o C to 50 o C)

BEYOND LINE-OF-SIGHT RANGE:

• 1.9 mi (3 km) integrated capability

• Extensible beyond 3.1 mi (5 km)

ALTITUDE:

• 1500 ft. (450 m) AGL, 15000 ft. (4500 m) MSL

LAUNCH & RECOVERY METHOD:

• Vertical Take-Off and Landing (VTOL)

DIMENSIONS:

• Deployed : 40 in. (102 cm) diameter,

9.3 in. (24 cm) height

• Folded : 20 in. (50 cm) length,

10 in. (25 cm) width

WEIGHT (WITHOUT PAYLOAD):

• 5.3 lbs (2.4 kg)

ADDITIONAL PAYLOADS:

• 3-axis stabilized high resolution EO camera • Custom payload development

NAVIGATION LEDS:

• Red/Green and Red/NIR

RADIO FREQUENCIES:

• 900 mhz, 2.4 GHz, custom

CONTROL AND DATA LINK:

• Low-latency all-digital network

SECURITY:

• Secure network pairing,

AES 256 bit encryption 

# MILITARY & GOVERNMENT APPLICATIONS

Anti-piracy, tactical ship boarding

De-mining

Emergency & disaster response

HAZMAT/CBRNE management

For information about Aeryon sUAS solutions, contact your Aeryon Sales Representative:

Call +1-519-489-6726 ext: 320 or email sales@aeryon.com

www.aeryon.com | @aeryonlabs