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GT-380 Remotely Piloted Aircraft System

Aircraft Specifications


Endurance: 4 hours
Cruise Speed: 90 knots
Max Speed: 180 kts
Max Ceiling: 10,000 feet
Normal Cruise Altitude: 1000 - 5,000 feet
Range: 100 nautical miles
Takeoff/Landing Speed: 35 knots
Max Payload Capacity: 25 lbs total


Type: Single Engine, Tractor, V-Tail
Engine: 62-150cc Single or Dual Cylinder (gasoline)
Construction: Modular, Compression Molded Composite
Landing Gear: Fixed or Retractable w/suspension
Wingspan: 8'7"
Length: 6'3"
Height: 2'9"
Weight (dry/no payload): 35 lbs
Weight (wet/no payload): 40 lbs
Weight (wet/payload): 65 lbs max
Gapless flight control surfaces
Generator (300 watts)
Trailing Edge Flaps
LED Navigation & Landing Lights
Reconfigurable for all autopilots
Forward Look Camera (FLC)
IR Night Landing System (IRNLS)(optional)

Payload Options

Centerline Fuselage Payload (15 lbs)
Wing Payload Stations (2) (optional - 5 lbs each)
Wing Fuel Tanks (optional)

GT Aeronautics GT380 RPAS GT Aeronautics GT380 RPAS

The GT-380 RPAS is a modular unmanned aircraft system designed to fulfill multi-role applications in the short field takeoff and landing environment. The aircraft incorporates multiple high-lift devices and "all-composite" construction to enable flight operations in confined rural and urban areas. With the high-lift devices stowed, the specially-designed laminar-flow airfoil allows the GT-380 to cruise in excess of 100 knots, reducing the "base to on-scene" flight time and extending its range. The fixed landing gear includes a rugged shock suspension system and steerable nosewheel, providing a robust capability in rough-field operations. Brakes are optional on the main wheels. The powerplant is an air-cooled, single cylinder engine. An optional powerplant is a dual cylinder engine that incorporates an electric starter for inflight start and a generator system capable of 300 watts of inflight power. An internal 1 gallon fuel supply and wing station fuel can provide endurance exceeding 3 hours and 100 nautical miles. On-site assembly, launch, and operation are accomplished with only 2 personnel in 30 minutes or less. The aircraft can launch and recover from semi-improved surfaces. The aircraft utilizes high-intensity LED and/or IR lighting for night operations. Night landings are performed using a portable IR night landing system.

NOTE: The performance specifications listed above are calculated. The GT-380 RPAS completed initial flight testing in July 2015 and will continue flight testing through 2016 to validate performance specifications.

GT AERONAUTICS, LLC, 26 Elk Road, Cody, WY 82414-7810, Phone & FAX: (307) 587-5221