OVERVIEW
The Jordan Falcon is a joint development effort intended to bring UAV capabilities to the Jordanian military.
The Jordan Falcon is a joint development effort intended to bring UAV capabilities to the Jordanian military.
YEAR: 2012
MANUFACTURER(S): King Abdulla D & D Bureau / Jordan Aerospace Industries - Jordan
PRODUCTION: 3
OPERATORS: Jordan
SPECIFICATIONS
Unless otherwise noted the presented statistics below pertain to the Jordan Falcon model. Common measurements, and their respective conversions, are shown when possible.
Unless otherwise noted the presented statistics below pertain to the Jordan Falcon model. Common measurements, and their respective conversions, are shown when possible.
CREW: 0
WEIGHT (EMPTY): 88 pounds (40 kilograms)
WEIGHT (MTOW): 132 pounds (60 kilograms)
ENGINE: 1 x 2-Stroke 200cc gasoline/oil mix engine powerign a two-bladed propeller in pusher configuration.
SPEED (MAX): 112 miles-per-hour (180 kilometers-per-hour; 97 knots)
RANGE: 280 miles (450 kilometers; 243 nautical miles)
ARMAMENT
None. Mission payload (up to 13lb) consisting of sensors and optical systems.
None. Mission payload (up to 13lb) consisting of sensors and optical systems.
VARIANTS
Series Model Variants
• Falcon - Base Series Designation
Series Model Variants
• Falcon - Base Series Designation
HISTORY
Detailing the development and operational history of the Jordan Falcon Light Reconnaissance Unmanned Aerial Vehicle (UAV). Entry last updated on 11/10/2016. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
Detailing the development and operational history of the Jordan Falcon Light Reconnaissance Unmanned Aerial Vehicle (UAV). Entry last updated on 11/10/2016. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
The Jordan Falcon in a light-class unmanned aerial vehicle (UAV) currently in development and headed by the concerns of King Abdulla Design & Development Bureau and Jordan Aerospace Industries. The effort is a joint venture indigenous UAV program intended to broaden the tactical reach of military and security forces - in an effort to modernize forces and keep pace with Western powers. The Falcon is an unarmed system, charged mainly with reconnaissance, surveillance and target designation/tracking and is therefore "armed" with applicable mission equipment for the role (payload of up to 13lbs).
Outwardly, the Jordan Falcon is designed as a small-scale aircraft to include a fuselage, main wing span and empennage. The "cockpit" is underslung in a nacelle-type arrangement at center with the straight-edged wings overhead. The wings are clipped at their tips. The empennage consists of a twin-boom configuration with a connecting span of wing at the rear, a horizontal tailplane that appears as two inward-canted vertical tail surfaces joined at their tips. Propulsion is from an internal engine situated at the rear of the fuselage and powering a twin-bladed propeller assembly in a "pusher" configuration. The undercarriage consists of four fixed legs.
As with other systems of this type, the Falcon sports a reduced-noise 200cc 2-stroke internal combustion engine and satellite-based navigation. The system is primarily controlled by a ground operator and range is out to 450 kilometers though waypoint navigation can be autonomous if required. A datalink system relays video in real-time format back to a receiver. Operational endurance time for the UAV is reported to be roughly four hours. Top speed is 110 miles per hour.
Outwardly, the Jordan Falcon is designed as a small-scale aircraft to include a fuselage, main wing span and empennage. The "cockpit" is underslung in a nacelle-type arrangement at center with the straight-edged wings overhead. The wings are clipped at their tips. The empennage consists of a twin-boom configuration with a connecting span of wing at the rear, a horizontal tailplane that appears as two inward-canted vertical tail surfaces joined at their tips. Propulsion is from an internal engine situated at the rear of the fuselage and powering a twin-bladed propeller assembly in a "pusher" configuration. The undercarriage consists of four fixed legs.
As with other systems of this type, the Falcon sports a reduced-noise 200cc 2-stroke internal combustion engine and satellite-based navigation. The system is primarily controlled by a ground operator and range is out to 450 kilometers though waypoint navigation can be autonomous if required. A datalink system relays video in real-time format back to a receiver. Operational endurance time for the UAV is reported to be roughly four hours. Top speed is 110 miles per hour.
MEDIA
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Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.
Relative Maximum Speed
Hi: 120mph
Lo: 60mph
This entry's maximum listed speed (112mph).
Graph average of 90 miles-per-hour.
City-to-City Ranges
NYC
LDN
LDN
PAR
PAR
BER
BER
MSK
MSK
TKY
TKY
SYD
SYD
LAX
LAX
NYC
Graph showcases the Jordan Falcon's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production (3)
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units
3
3
