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AAI RQ-7 Shadow Print E-mail



The RQ-7 Shadow unmanned aerial vehicle (UAV) is used by the United States Army and Marine Corps.

Launched from a rail, it is recovered with the aid of arresting gear similar to jets on an aircraft carrier.
The RQ-7 Shadow is the result of a continued US Army search for an effective battlefield UAV after the cancellation of the RQ-6 Outrider aircraft. AAI followed up their RQ-2 Pioneer UAV with the similar but refined Shadow 200, and in late 1990 the Army selected the Shadow 200 to fill the tactical UAV requirement, redesignating it the RQ-7. The Army requirement specified a UAV that used a gasoline engine, could carry an electro-optic/infrared imaging sensor turret, and had a minimum range of 31 miles (50 kilometers) with four hour endurance on station. The Shadow 200 offered at least twice that range, powered by a 38 hp (28.5 kW) rotary engine. The Army requirement dictated that it be able to land in a soccer field.
In 2007, the United States Marine Corps began to transition from the RQ-2 Pioneer to the RQ-7 Shadow.
Production of Shadow aircraft shifted to a generally improved RQ-7B variant in the summer of 2004. The RQ-7B features new wings increased in span by 91.4 centimeters (36 inches); the new wings are not only more aerodynamically efficient, they are "wet" to increase fuel storage for greater range and endurance.
Endurance has been increased to 6 hours, and payload capability has been increased to 45 kilograms (100 pounds). After reports from Iraq that engines were failing, in 2005, the Army's UAV project manager called for the use of 100LL, an aviation fuel, rather than the conventional 87 octane mogas. Avionics systems have been generally improved, and the new wing is designed to accommodate a Communications Relay Package, which allows the aircraft to act as a relay station. This allows commanders or even the aircraft operators themselves to communicate via radio to the troops on ground in locations that would otherwise be "dead" to radio traffic.

Specifications :
General characteristics :

* Length: 11.2 ft in (3.41 m)
* Wingspan: 14 ft in (3.87 m)
* Height: 3.3 ft in (1 m)
* Empty weight: 186 lb (77 kg)
* Gross weight: 375 lb (170 kg)
* Powerplant: × 1 Wankel UAV Engine 741 used only with Silkolene Synthetic Oil, 38 hp (28.5 kW) each
Performance :
* Range: 68 miles (109.5 km)
* Endurance: 6 hours
* Service ceiling: 15,000 ft (ELOS (Electronic Line Of Sight) m)