Outwardly, the Rustom prototype shares an appearance not unlike a Burt Rutan light aircraft design. It sports a three-legged, fixed undercarriage, rear-mounted main wing appendages and a canard wing assembly at front. Vertical fins are set at the main wing tips. The powerplant is contained in the aft section of the fuselage driving a two-bladed propeller in a "pusher" configuration. Avionics and mission equipment are housed within the forward section of the fuselage. The payload limit is listed at 165lbs while the empty airframe weighs 1,560lbs. Power is served through an American Lycoming O-320 series 4-cylinder engine of 150 horsepower.
The Rustom-H shares a wholly different physical configuration than the Rustom-I prototype as it sports mid-set, straight main wing appendages, a bulbous nose section (ala the Northrop Grumman Global Hawk), a retractable, three-legged undercarriage and a tapering empennage. The tail unit is of a conventional "T" shape with its high-mounted horizontal tailplane. The payload limit is 770lbs with an empty airframe weight of 4,000lbs while power is served through 2 x Russian NPO-Saturn 36MT series turboprop engines fitted under the wings in nacelles, these engines developing 100 horsepower each while driving three-bladed propellers. The Rustom-H is scheduled for a first flight in 2014.
The Rustom features a maximum speed value of 140 miles per hour with a range out to 220 miles (Rustom-I) and 625 (Rustom-H). The Rustom-I will operate at altitudes of up to 26,000 feet while the Rustom-H will operate closer to 35,000 feet. No specifications are currently available for the Rustom-II UCAV.
As of this writing (December 2013), the Rustom is in active development. The series is intended to replace the Israeli-originated, globally popular IAI "Heron" line of unarmed UAVs in service with the Indian Air Force and Indian Navy.
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