A General Atomics Aeronautical Systems Gray
Eagle unmanned aircraft system has performed manned-unmanned teaming with a
Boeing AH-64 Apache helicopter (shown here during a trial in South Korea in
2015). (GA-ASI)
As the Army continues to develop its multidomain battle
concept, manned-unmanned teaming will play a large role in operations going
forward.
Despite multidomain battle being a new, updated vision to
how the Army fights conflicts, the service has been conducting manned-unmanned
teaming, or MUM-T, for some time, most notably involving Apache attack
helicopter pilots being able to control MQ-1C Gray Eagles.
The retirement of the Army’s OH-58 Kiowa Warrior scout
helicopter left the service with a capability gap, so “the Army came up with
[this idea that] we’re going to use our unmanned aerial systems to do that,”
Chris MacFarland, General Atomics Aeronautical Systems Inc. director of Army
programs, told C4ISRNET in an interview.
GA-ASI manufactures the Gray Eagle, as well as the Air
Force variants the MQ-1 Predator and the larger MQ-9 Reaper.
Apache aircraft have used MUM-T systems in battlefield
situations with great success in Iraq and Afghanistan, according to a spokesman
from the Army’s Program Executive Office Aviation.
Moreover, the spokesman added that the AH-64E Apache is
fully digitized with the latest technologies including level 4 man-unmanned
teaming that allows Apache pilots to control flight path and payloads of
unmanned aircraft system including the Gray Eagle. Level 4 MUM-T allows an
Apache copilot gunner to not only receive live sensor imagery from an unmanned
aircraft, but also take control of the sensor and weapons payloads and the
aircraft navigation via waypoint management, according to Grant Taylor,
engineering research psychologist for the Army Aviation Development
Directorate..........Read rest of article: HERE
MQ-1C Gray Eagle
The MQ-1C Gray Eagle is powered by a single Thielert 2.0L
heavy-fuel piston engine with 165 hp and provides an unmanned long-endurance
and persistent ISR and tactical strike capability. The MQ-1C performs the following
missions: Reconnaissance, Surveillance, Target Acquisition (RSTA), command and
control, communications relay, signals intelligence (SIGINT), battle damage
assessment, and manned-unmanned teaming capability. The Gray Eagle has a
wingspan of 56 feet, is 28 feet long, and carries a payload of up to 1,075
pounds. The Gray Eagle is equipped with the Raytheon AN/AAS-53 Common Sensor
Payload (CSP), which includes Electro-Optical/Infrared (EO/IR) video cameras
and laser designators. The MQ-1C also features a Synthetic Aperture Radar
(SAR), communications relay, and carries up to four AGM-114 Hellfire missiles.
Source: fi-aeroweb.com
MIL-SPEC: Gray Eagle
Manufacturer: General Atomics Aeronautical Systems (GA-ASI)
Max. altitude: 29,000 feet
Max. endurance: More than 30 hours
Max. air speed: 135 knots true airspeed (approximately 155 mph)
Payload: 1,075 pounds
Engine: Thielert Centurion inline-four piston turbodiesel
Displacement: 2.0L (121.5 ci)
Bore: 3.26 inches (83 mm)
Stroke: 3.62 inches (92 mm)
Compression: 18:1
Dimensions (WxLxH): 30.63 x 32.12 x 25.04 inches (778 x 816 x 636 mm)
Manufacturer: General Atomics Aeronautical Systems (GA-ASI)
Max. altitude: 29,000 feet
Max. endurance: More than 30 hours
Max. air speed: 135 knots true airspeed (approximately 155 mph)
Payload: 1,075 pounds
Engine: Thielert Centurion inline-four piston turbodiesel
Displacement: 2.0L (121.5 ci)
Bore: 3.26 inches (83 mm)
Stroke: 3.62 inches (92 mm)
Compression: 18:1
Dimensions (WxLxH): 30.63 x 32.12 x 25.04 inches (778 x 816 x 636 mm)
Thielert Centurion inline-four 2.0L piston turbodiesel
Weight (complete and dry): 295.4
pounds (134 kg)
Power: 135 hp (recommended load: 75 percent)
Torque: 302 lb-ft
Max. rpm: 4,500 rpm
Fuel consumption: 0.35 lb/hphr
Fuel type: Diesel (EN590), Jet A, JP-8, Chinese Jet Fuel No. 3
Valvetrain: Dual overhead camshaft (DOHC)
Fuel Injection system: Common-rail direct injection
Cooling: Liquid
Oil system: Wet sump
Pop drive: Reduction gearbox with integrated clutch
Propeller: Three-blade with hydraulic variable pitch
Engine lifetime: 1,500 hours
Power: 135 hp (recommended load: 75 percent)
Torque: 302 lb-ft
Max. rpm: 4,500 rpm
Fuel consumption: 0.35 lb/hphr
Fuel type: Diesel (EN590), Jet A, JP-8, Chinese Jet Fuel No. 3
Valvetrain: Dual overhead camshaft (DOHC)
Fuel Injection system: Common-rail direct injection
Cooling: Liquid
Oil system: Wet sump
Pop drive: Reduction gearbox with integrated clutch
Propeller: Three-blade with hydraulic variable pitch
Engine lifetime: 1,500 hours
Source: trucktrend.com
No comments:
Post a Comment