The Super Galeb sports a modern appearance. She holds a rather short nose cone with the cockpit situated just aft. The stepped cockpit features seating for two personnel in tandem - a student in the forward seat and an instructor in the rear seat when used in the advanced trainer role. The cockpit canopy is a multi-piece unit with individual systems for each pilot as well as a framed forward component. Ejection seats are afforded to both positions. A raised spine behind the cockpit area disrupts views to the "six" angle. Intakes are mounted along the sides of the fuselage and aspirate the single turbojet engine. Wings are low-mounted assemblies fitted approximately amidships in the design. The wings sport sweep along the leading edge, features cut-off rounded wingtips and have slight sweep along the trailing edge. The empennage is conventional and makes use of a single vertical tail fin with a pair of all-moving horizontal tailplanes mounted at its base, each sporting anhedral. The engine exhausts through a circular ring at the rear of the fuselage and base of the vertical tail fin. Her undercarriage is a traditional tricycle arrangement featuring two main single-wheeled landing gear legs and a single-wheeled nose landing gear leg.
Performance and Dimensions
The G-4 is powered by a single engine buried within the elegant fuselage. The engine itself is of British origin, a license-produced Rolls-Royce Viper Mk 632-46 series turbojet system delivering up to 4,000lbs of thrust. Her top speed is billed at 565 miles per hour while her range is limited to 1,553 miles. The G-4 maintains a service ceiling in the neighborhood of 42,160 feet and sports a rate of climb equal to 6,100 feet per minute. Dimensionally, the G-4 features a wingspan of 32 feet, 5 inches and a running length of 37 feet, 2 inches. Her sitting height is just over 14 feet. The aircraft fields an empty weight of 6,993lbs and boasts a maximum take-off weight (MTOW) near 13,889lbs.
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