Design and development
The airframe, constructed of aluminium alloy with steel used in highly stressed parts, resembled a large Il-28, the long fuselage having swept tail surfaces, and a similar arrangement of cockpits for the crew of pilot, navigator and rear gunner. The wing, which had moderate taper but straight leading edges, copied the layout of the Il-28, being mounted in the shoulder position at the midpoint of the fuselage. The flying controls consisted of the usual ailerons, elevators and rudder, all fitted with trim tabs for reducing loads on the pilots controls during flight in steady states, as well as "reversible" hydraulically-powered actuators.[1]
Two Lyul'ka AL-5 engines were fitted in long nacelles forward of the wings, exhausting through long jetpipes at the rear of the nacelles, aft of the wing trailing edge. The engines were mounted in this fashion to make room for the retracted main undercarriage legs, two on each side attached to the engine nacelles under the wings. The paired main undercarriage legs, side by side, retracted in opposite directions, inboard forwards and outboard rearwards, with the single mainwheels rotating 90 degrees to lie flat under the long jetpipes of the AL-5 engines. To boost takeoff performance, two JATO bottles could be attached to the rear fuselage. Performance was also improved when Lyulka AL-5F (forseerovannyy - afterburning) engines were fitted.[1]
Flight tests and state acceptance trials were successful, with the Il-46 meeting all requirements. Production was not ordered because the Tupolev Tu-88 proved to have better performance, and was ordered into production as the Tu-16.[1]
The Il-46S swept-wing version was designed concurrently, but construction was not started, to ensure that resources were not diverted from the Il-46.[1]
