Sidewinder

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The Sidewinder Unmanned Aircraft System (UAS) is a high altitude, multi fuel, intelligence, surveillance and reconnaissance (ISR) asset. Capitalizing on the capabilities of today’s micro turbine engines, we have produced a class II vehicle capable of high altitudes (25,000 feet +), wide speed ranges, and heavy fuel burning, operating in a low vibration environment for ISR payloads as well as experimentation instruments. With more capability than a standard two-stroke piston engine, the Sidewinder can use various heavy fuels including diesel, kerosene and Jet A. The Sidewinder UAS is controlled by the UAV Solutions Portable Ground Control System integrated with a tracking antenna.

• Open architecture layout for various communication links and payloads
• Autonomous operation with operator guided modes
• Rolling take-off; retractable landing gear with hydraulic brakes
• 80 lb. thrust turbine engine
• Fuel capacity up to 15 gallons (extended tanks will be available)
• Aircraft grade aluminum and carbon fiber construction
• Hard points integrated for external stores
• Field proven avionics with thousands of hours of operation
• Ideal for ISR, experimentation and as a target drone

Length: 12’ 4”
Wingspan: 16’
MGTOW: 300 lbs.
Endurance: 2.5 hours max
Payload Capacity: 10 lbs.
Stall Speed: 45 knots
Cruise Speed: 65-75 knots
Dash Speed: 120 knots
Communications: 3 00 MHz, 900 MHz, 2.4 GHz or 5.8 GHz C2 and video

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Intruder

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The Intruder Unmanned Aircraft System (UAS) is a multiple intelligence gathering platform with larger volume bays, long endurance and higher altitude capabilities. Not only can the Intruder fly heavy payloads but unlike other platforms, provides the volume to house them. This versatile system utilizes intelligence gathering disciplines to collect information via satellite communication (SATCOM), signals intelligence (SIGINT), communications intelligence (COMINT) and imagery intelligence (IMINT). A muffled tractor engine configuration provides the aircraft with greater propulsion efficiency and noise reduction. Composite construction allows for a more aerodynamic design, and removable wing sections allow for easy hangar storage without full disassembly. The Intruder has a retractable landing gear to reduce drag and noise signature during cruise. An agnostic, center-of-gravity mounted payload location accommodates from 75 to 100 lbs. UAV Solutions ground control systems (GCS) – both the Portable GCS and Tactical GCS – can be used to operate the Intruder for remote operations.

• Open architecture layout for payload and communication link flexibility
• Expansive volumes and multiple locations for larger dimension and multi-payload capability
• Field proven avionics with thousands of hours of operation
• 50 HP twin cylinder fuel injected engine
• Low noise signature
• Fuel capacity up to 27 gallons (expandable)
• Rolling take-off; retractable landing gear with hydraulic brakes
• Aircraft grade aluminum and carbon fiber construction
• Hard points integrated for external stores
• Ideal for ISR, multi-int and experimentation

Length: 16’
Wingspan: 30’
MGTOW: 850 lbs.
Endurance: 12 hours max
Payload Capacity: 75-100 lbs.
Cruise Speed: 75 knots
Stall Speed: 50 knots
Communications: 3 00 MHz, 900 MHz, 2.4 Ghz or 5.8 GHz C2 and video, SATCOM also available

 

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Portable Ground Control System

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UAV Solutions, Inc. (UAVS) designs and builds the Portable Ground Control System (GCS) and the Tactical Ground Control System to control our internally developed unmanned aircraft systems (UAS) as well as UAS platforms designed by other manufacturers. Our GCS provides the user command and control of payloads, mission planning and real time video. The Portable GCS and Tactical GCS can be networked into existing command center networks for video distribution and metadata streams. Equipped with a powerful embedded onboard processor, operators can rapidly receive the vital intelligence they require to complete their mission. Our systems have been created with the user in mind.

Exterior Dimensions47.2”x16.5”x9.2”
Weight : 70 lbs.
Case Features : Two soft-grip handles, in-line wheels
Input Power : A/C 110
Connections : 6 USB, 4 Ethernet
Selectable Video Output : √
CPU Power Switch : √
Embedded CPU : Windows 7 PRO, 4GB RAM
Displays : Three (3) 17” TFT LCD; 2 computer/mission planning and 1 raw video

The Portable GCS is ideal for multiple crew members operating larger air vehicles. The addition of a tracker antenna enables autonomous tracking of the air vehicle and extends the search range.

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Tactical Ground Control System

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UAV Solutions, Inc. (UAVS) designs and builds the Portable Ground Control System (GCS) and the Tactical Ground Control System to control our internally developed unmanned aircraft systems (UAS) as well as UAS platforms designed by other manufacturers. Our GCS provides the user command and control of payloads, mission planning and real time video. The Portable GCS and Tactical GCS can be networked into existing command center networks for video distribution and metadata streams. Equipped with a powerful embedded onboard processor, operators can rapidly receive the vital intelligence they require to complete their mission. Our systems have been created with the user in mind.

Exterior Dimensions : 21.5”x16.5”x9.2”
Weight : 35 lbs
Case Features : One soft-grip handle,
Electrical Specifications : integrated antenna mount
Input Power : A/C 110
Connections : 3 USB, 2 Ethernet
Selectable Video Output : N/A
CPU Power Switch : √
Embedded CPU : Windows 7 PRO, 4GB RAM
Displays  : Two (2) 17” TFT LCD; 1 computer/mission planning &1 Ethernet video

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Phoenix AG

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The Phoenix Ag is one of the first unmanned vertical take-off and landing (VTOL) systems designed especially for the agriculture market. The fully integrated MicaSense RedEdge™ camera provides accurate multi-band data for agricultural remote sensing applications. Information can be collected at resolutions measured in just inches per pixel to map the health of crops over time. A system consists of the air vehicle with an integrated RedEdge camera, batteries, charger, laptop ground control system with communications radios, video display and spare parts – all in one convenient carrying case. The VTOL aspect allows the air vehicle to operate in tight spaces.

Features
• Two- axis mechanically stabilized nadir position gimbal camera
• Gimbal integrated with MicaSense RedEdge multispectral camera
• Standard nose mount camera for situational awareness-transmits over5.8G analog radio
• Fully autonomous system with multiple user modes
• Open architecture systems
• Comprehensive Operations and Maintenance Manuals including
maintenance schedule and troubleshooting guide
• Section 333 paperwork available

Length: 34”
Width: 27.6”
MGTOW: 8 lbs.
Endurance: 35 – 40 minutes
Typical Operating Altitude: 50-500 ft. AGL

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Dragon View

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Combined Electro-optic/Infrared; Pan-Tilt-Zoom

Can be Integrated on Air Vehicles, Towers and
Other Infrastructure

Mechanically and Digitally Stabilized

Video Processing and Object Tracking

Operating at 24 Watts: Makes Battery More Efficient for Longer Duration

Weight: 1.60 lbs.; VIN: 24V

Standard Ethernet Interface

Digitally Compressed Video Output – H.264

Onboard Video Recording to Micro SD Card

Video Stabilization

In-frame Object Tracking (in development)

Integrated Inertial Measurement Unit (IMU)
for Rate Feedback

Slow rate version is Non-ITAR controlled

Configurable to Your Application

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Phoenix 60LE

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Rugged VTOL Hexacopter Unmanned Aircraft System – Foldable booms

Ideal for Military, Police and First Responders

Ready to Launch in 10 Minutes

Combined stabilized color and thermal imager payload

Comprehensive Operations and Maintenance Manual includes maintenance schedule and troubleshooting guide

Length x Width: 40” x 40”

Empty Weight: 20.8 lbs.

MGTOW: 40 lbs. (manual says 30.4)

Payload Capacity: 3-8 lbs.

Range: 2-3 miles LOS

Endurance: 25-50 minutes (depending on battery/payload configuration)

Maximum Speed: 24 knots

Cruise Speed: 15.5 knots

Typical Operating Altitudes: 50-500 ft. AGL: MSL to 10,000 ft.

Propulsion: One (1) 22,000mAh Li-Po Battery

Communications: 900 MHz Command and Control; 2.4 GHz Digital Data Link Video

Weather: Flies in 1 inch-an-hour of rain; can fly in light snow, light dust/dust storms; 25 knot gusts; 15-17 knots sustained winds

Autopilot: UAVS Open Source

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Phoenix 60

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Rugged VTOL Hexacopter Unmanned Aircraft System – Foldable booms

Ideal for Military, Police and First Responders

Ready to Launch in10 Minutes

Combined stabilized color and thermal imager payload

Comprehensive Operations and Maintenance Manual includes maintenance schedule and troubleshooting guide

Length x Width: 30” x 30”

Empty Weight: 10.4 lbs

MGTOW: 15 lbs. (or is it closer to 17.4 lbs)

Payload Capacity: 3 lbs.

Range: 2 miles LOS

Endurance: 30-35 minutes

Maximum Speed: 24 knots

Cruise Speed:15.5 knots

Typical Operating Altitudes: 50-500 ft. AGL: MSL to 10,000 ft.

Propulsion: One (1) 22,000mAh Li-Po Battery

Communications: 900 MHz Command and Control; 2.4 GHz Digital Data Link Video

Weather: Flies in 1 inch-an-hour of rain; can fly in light snow, light dust/dust storms; 25 knot gusts; 15-17 knots sustained winds

Autopilot: UAVS Open Source

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Phoenix 30

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Rugged VTOL Quadcopter Unmanned Aircraft System – Foldable booms

Ideal for Military, Police and First Responders

Ready to Launch in 10 Minutes

Combined stabilized color and thermal imager payload

Comprehensive Operations and Maintenance Manual includes maintenance schedule and troubleshooting guide

Length x Width: 20” x 20”

Empty Weight: 6.2 lbs.

MGTOW: 12 lbs.

Payload Capacity: 2 lbs.

Range: 2 miles LOS

Endurance: 35-40 minutes

Maximum Speed: 24 knots

Cruise Speed: 15.5 knots

Typical Operating Altitudes: 50-500 ft. AGL: MSL to 10,000 ft.

Propulsion: One (1) 22,000mAh Li-Po Battery

Communications: Dual 900 MHz Command and Control; 2.4 GHz Digital Data Link Video

Weather: Flies in 1 inch-an-hour of rain; can fly in light snow, light dust/dust storms; 25 knot gusts; 15-17 knots sustained winds

Autopilot: UAVS Open Source

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Talon 240G

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Gas version; Electronic Fuel Injected (EFI) Engine

Developed for military and commercial use
– built from 7075 aircraft grade aluminum and composite materials

Capable of carrying a multitude of EO/IR sensors or other payloads (Multi-spectral and other ISR)

Open architecture philosophy for software and hardware components; provides customers with flexibility for future product enhancement

Fully autonomous system with multiple user modes

Comprehensive Operations and Maintenance Manual includes maintenance schedule and troubleshooting guide

Wingspan: 20’; Length: 9’6”

Empty Weight: 120 lbs.

Fuel Volume: 27 lbs.

MGTOW: 172 lbs.

Payload Capacity: 25 lbs.

Launch/Recovery: Rolling take-off; Fixed landing gear option; less than 800 ft. of grass of equivalent runway required; Other Options: truck or catapult launch; belly recovery

Range: 8-40 miles LOS (depending on communications)

Endurance: 6-10 hours

Maximum Speed: 50 knots

Cruise Speed: 37 knots

Typical Operating Altitudes: 50-5,000 ft. AGL: MSL to 12,000 ft.

Propulsion: AvGas; reciprocating, tractor configuration, DA-120, Fuel injected

Communications: 300/900 MHz Command and Control; 2.4 GHz Digital Data Link Video

Weather: Flies in 1/2 inch-an-hour of rain; can fly in light snow, light dust/dust storms; 25 knot gusts; 15-17 knots sustained winds

Autopilot: UTC/Cloud Cap Technology

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