AgEagle RX40

AgEagle

Drone for precision agriculture mapping

Snapshot
Manufacturing & delivery
Performance & use
Research & standards
Feedback

Product description Brand name and product description

AgEagle RX40 is a professional drone that captures aerial maps for precision agriculture growers

Target region(s) Target region for distribution/implementation (listed by country if specified)

Brazil, Ukraine and the US

Distributors/implementing organizations Organization(s) distributing/deploying this product directly to communities/individuals?"

AgEagle Aerial Systems

Market suggested retail price Price per unit or service price per usage/terms (USD). Subsidies noted.

$4,995 – $8,766 depending on the model

Competitive landscape Similar products available on the market. May not be a comprehensive listing.

Wings for Aid
Drones for Development Dr.One
HoneyComb

SDG targeted United Nations Sustainable Development Goals (SDGs) targeted with this product/application/service

Goal 2: End hunger, achieve food security and improved nutrition and promote sustainable agriculture

Target user(s) Target user/consumer base (country, income segment)

Precision agriculture growers

Manufacturing/building method(s) Detail regarding solution production or construction method (instructions, mass production capacity, custom made,etc...)

Designed and built in the US using “Tractor Tough” airframes

Product Intellectual Property Open source/IP protected (note patent)/trade secret/other?

Copyrighted 2013 AgEagle Aerial Systems

User Provision Model Where can the product be purchased/acquired by end users?

Direct sales and authorized dealers

Distribution to date Number of units that have been deployed, downloads or users to date

Unknown

Fields marked are sourced values that have been evaluated by the manufacturer or a third party, all others are design specifications.

Drone type

List type of drone (Fixed wind, quad copter, other

)

Fixed Wing (Flying Wing)

Weight (kg)

1.95

Take off / Landing type

Vertical, runway, catapult, hand launched, other

Hand launch / Auto landing, power off glide

Carry case dimensions (m)

Unknown

GNSS system

List the navigation system (GPS, GLONAS, Galileo, BeiDou, other)

Dual GPS (L 1 /L 2 & Glonass) NEO8

Flight time (hour)

Max flight time, coverage area, etc

44 mins

Cruise speed (km per hour)

53.1

Battery type

One Li-Po Battery (6600 mAh; 14.8V; 10C; 4 Cell)

Sensors available (Y/N)

If yes, specify the type of sensors included and available for the platform

Barometric Altimeter, Airspeed Indicator, 2 x Accelerometer, 2 x Gyroscope, 2 x Magnetometer, GPS, Glonass

Type of data collected

Geolocation, Land Survey, Sensor readings, Image based data, OtherDisplay order

Pictures (Resolution 10.830 cm / pixel size at 121.92 m AGL

Drone software platform

List the drone tracking and management software specificationsDisplay order

Android tablet app

Application

Objective of the drone platform [eAgriculture, Land survey, Disaster response, Impact analysis, Wildlife tracking, other]Display order

Agricultural mapping

Design specifications Component and Operation overview including power, portability, facility requirements, preventative maintenance and user training requirements

No internet required to operate
Pre-programmed missions
No launcher required
Botlink NIRX image processing
Flying in wind conditions that hamper quad copters
True NIR images from the Sentera NDVI Single Sensor
Composite construction with hardened points for longevity and reliability

Product schematics Design and assembly illustrations

Composition: Composite/EPP/Carbon Fiber Rod
Measurements: Wingspan: 47″ (120 cm)
Weight: Max Gross T.O.: 4.4 lb (2 kg)
Fuel/Energy System: Single Li-Po, 6600 mAh; 14.8V; 10C; 4 Cell
Take-Off Method: Manual
Landing Method: Belly Landing
Flight Performance: Operating Airspeed: 31-36 mph (13.8-16 m/s)
Endurance: Up to 50 mins. w/ Std. Batteries

Technical support Technical support provided by

Local support from AgEagle dealers

Replacement components Availability of replacement components (in-country, by order,...)

Available online

Lifecycle Disposal and warranty

One or two years repair and replacement plans available for an extra charge

Manufacturer specified performance targets Designer / Manufacturer specified targets

Operating Airspeed: 31-49 mph (13.8-22 m/s)
Cruise Airspeed: 33 mph (14.7 m/s)
Max Descent Rate: 394 ft./min (2 m/s)
Max Climb Rate: 984 ft./min (5 m/s)
Max Turn Rate: 150 deg/s
Endurance: 60 mins. w/ Std. Batteries

Vetted performance Findings of manufacturer evaluations or independent testing centers

Unknown

Testing organizations Independent lab, academic research centers, etc.

Partido State University (Philippines)

Safety Potential hazards / risks related to operation of this product

Safety information included in the user manual

Complementary technical systems Performance of this product is improved with another technology (eg. Cookstoves and Wind-blocking skirts)

Catapult launcher for fixed wing drone

Academic research Academic research related to the product (e.g. published papers in peer-reviewed journals)

Charles M. Boozer, Michael J. Van Tooren, and Ali Elham. “Multidisciplinary Aerodynamic Shape Optimization of a Composite Blended Wing Body Aircraft“, 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA SciTech Forum, (AIAA 2017-0128)
https://doi.org/10.2514/6.2017-0128
Atole, R., Belo, L. and Lirang, J. “Eyes in the Sky: A Review of Civilian Unmanned Aerial Vehicles (UAVs)” , International Journal of Computer Applications (0975 – 8887) Volume 173 – No.6, September 2017
Moskvitch, K. “Take off: are drones the future of farming?“, IET Volume 10, Issue 7, August 2015, p. 62 – 66
I. Petkovics, J. Simon, Á. Petkovics and Z. Čović, “Selection of unmanned aerial vehicle for precision agriculture with multi-criteria decision making algorithm,” 2017 IEEE 15th International Symposium on Intelligent Systems and Informatics (SISY), Subotica, 2017, pp. 000151-000156.
doi: 10.1109/SISY.2017.8080543
Dehaan, R. “Evaluation of Unmanned Aerial Vehicle (UAV)-Derived imagery for the detection of Wild Radish in Wheat” December 2015

Compliance with regulations Product certifications and standards referenced by designer/manufacturer

Compliance with US FAA regulation

Evaluation methods Evaluation methods/protocols/guidelines referenced by designer or manufacturer.

Academic research

Other information

6. User Manuals

In context photographs (0)

You can use the form below to contribute a photo of this product.

In context files & documents (0)

Feedback from users, customers & distributors

Please let us know your experience in using this product through comments below.

Snapshot

Product description Brand name and product description

AgEagle RX40 is a professional drone that captures aerial maps for precision agriculture growers

Target region(s) Target region for distribution/implementation (listed by country if specified)

Brazil, Ukraine and the US

Distributors/implementing organizations Organization(s) distributing/deploying this product directly to communities/individuals?"

AgEagle Aerial Systems

Market suggested retail price Price per unit or service price per usage/terms (USD). Subsidies noted.

$4,995 – $8,766 depending on the model

Competitive landscape Similar products available on the market. May not be a comprehensive listing.

Wings for Aid
Drones for Development Dr.One
HoneyComb

SDG targeted United Nations Sustainable Development Goals (SDGs) targeted with this product/application/service

Goal 2: End hunger, achieve food security and improved nutrition and promote sustainable agriculture

Target user(s) Target user/consumer base (country, income segment)

Precision agriculture growers

Manufacturing & delivery

Manufacturing/building method(s) Detail regarding solution production or construction method (instructions, mass production capacity, custom made,etc...)

Designed and built in the US using “Tractor Tough” airframes

Product Intellectual Property Open source/IP protected (note patent)/trade secret/other?

Copyrighted 2013 AgEagle Aerial Systems

User Provision Model Where can the product be purchased/acquired by end users?

Direct sales and authorized dealers

Distribution to date Number of units that have been deployed, downloads or users to date

Unknown

Performance & use

Fields marked are sourced values that have been evaluated by the manufacturer or a third party, all others are design specifications.

Drone type

List type of drone (Fixed wind, quad copter, other

)

Fixed Wing (Flying Wing)

Weight (kg)

1.95

Take off / Landing type

Vertical, runway, catapult, hand launched, other

Hand launch / Auto landing, power off glide

Carry case dimensions (m)

Unknown

GNSS system

List the navigation system (GPS, GLONAS, Galileo, BeiDou, other)

Dual GPS (L 1 /L 2 & Glonass) NEO8

Flight time (hour)

Max flight time, coverage area, etc

44 mins

Cruise speed (km per hour)

53.1

Battery type

One Li-Po Battery (6600 mAh; 14.8V; 10C; 4 Cell)

Sensors available (Y/N)

If yes, specify the type of sensors included and available for the platform

Barometric Altimeter, Airspeed Indicator, 2 x Accelerometer, 2 x Gyroscope, 2 x Magnetometer, GPS, Glonass

Type of data collected

Geolocation, Land Survey, Sensor readings, Image based data, OtherDisplay order

Pictures (Resolution 10.830 cm / pixel size at 121.92 m AGL

Drone software platform

List the drone tracking and management software specificationsDisplay order

Android tablet app

Application

Objective of the drone platform [eAgriculture, Land survey, Disaster response, Impact analysis, Wildlife tracking, other]Display order

Agricultural mapping

Design specifications Component and Operation overview including power, portability, facility requirements, preventative maintenance and user training requirements

No internet required to operate
Pre-programmed missions
No launcher required
Botlink NIRX image processing
Flying in wind conditions that hamper quad copters
True NIR images from the Sentera NDVI Single Sensor
Composite construction with hardened points for longevity and reliability

Product schematics Design and assembly illustrations

Composition: Composite/EPP/Carbon Fiber Rod
Measurements: Wingspan: 47″ (120 cm)
Weight: Max Gross T.O.: 4.4 lb (2 kg)
Fuel/Energy System: Single Li-Po, 6600 mAh; 14.8V; 10C; 4 Cell
Take-Off Method: Manual
Landing Method: Belly Landing
Flight Performance: Operating Airspeed: 31-36 mph (13.8-16 m/s)
Endurance: Up to 50 mins. w/ Std. Batteries

Technical support Technical support provided by

Local support from AgEagle dealers

Replacement components Availability of replacement components (in-country, by order,...)

Available online

Lifecycle Disposal and warranty

One or two years repair and replacement plans available for an extra charge

Manufacturer specified performance targets Designer / Manufacturer specified targets

Operating Airspeed: 31-49 mph (13.8-22 m/s)
Cruise Airspeed: 33 mph (14.7 m/s)
Max Descent Rate: 394 ft./min (2 m/s)
Max Climb Rate: 984 ft./min (5 m/s)
Max Turn Rate: 150 deg/s
Endurance: 60 mins. w/ Std. Batteries

Vetted performance Findings of manufacturer evaluations or independent testing centers

Unknown

Testing organizations Independent lab, academic research centers, etc.

Partido State University (Philippines)

Safety Potential hazards / risks related to operation of this product

Safety information included in the user manual

Complementary technical systems Performance of this product is improved with another technology (eg. Cookstoves and Wind-blocking skirts)

Catapult launcher for fixed wing drone

Research & standards

Academic research Academic research related to the product (e.g. published papers in peer-reviewed journals)

Charles M. Boozer, Michael J. Van Tooren, and Ali Elham. “Multidisciplinary Aerodynamic Shape Optimization of a Composite Blended Wing Body Aircraft“, 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, AIAA SciTech Forum, (AIAA 2017-0128)
https://doi.org/10.2514/6.2017-0128
Atole, R., Belo, L. and Lirang, J. “Eyes in the Sky: A Review of Civilian Unmanned Aerial Vehicles (UAVs)” , International Journal of Computer Applications (0975 – 8887) Volume 173 – No.6, September 2017
Moskvitch, K. “Take off: are drones the future of farming?“, IET Volume 10, Issue 7, August 2015, p. 62 – 66
I. Petkovics, J. Simon, Á. Petkovics and Z. Čović, “Selection of unmanned aerial vehicle for precision agriculture with multi-criteria decision making algorithm,” 2017 IEEE 15th International Symposium on Intelligent Systems and Informatics (SISY), Subotica, 2017, pp. 000151-000156.
doi: 10.1109/SISY.2017.8080543
Dehaan, R. “Evaluation of Unmanned Aerial Vehicle (UAV)-Derived imagery for the detection of Wild Radish in Wheat” December 2015

Compliance with regulations Product certifications and standards referenced by designer/manufacturer

Compliance with US FAA regulation

Evaluation methods Evaluation methods/protocols/guidelines referenced by designer or manufacturer.

Academic research

Other information

6. User Manuals

Feedback

In context photographs (0)

You can use the form below to contribute a photo of this product.

In context files & documents (0)

Feedback from users, customers & distributors

Please let us know your experience in using this product through comments below.

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In context photographs (0)

In context files & documents (0)

Feedback from users, customers & distributors