Bell 309 KingCobra

• Name — Bell 309 KingCobra • Type — Attack helicopter prototype • Manufacturer — Bell Helicopter • First Flight — 10 September 1971 (Twin-engine) January 1972 (Single engine) • Primary User — United States Army • Number Built — 2 • Developed From — Bell AH-1 Cobra

The AH-1 Cobra was developed in the mid-1960s as an interim gunship for the U.S. Army for use in Vietnam. The Cobra shared the proven transmission, rotor system, and the T53 turboshaft engine of the UH-1 "Huey". By June 1967, the first AH-1G HueyCobras had been delivered. Originally designated as UH-1H, the "A" for attack designation was soon adopted and when the improved UH-1D became the UH-1H, the HueyCobra became the AH-1G. Bell built 1,116 AH-1Gs for the US Army between 1967 and 1973, and the Cobras chalked up over a million operational hours in Vietnam. The US Army purchased the AH-1G as an "interim type" for the "jungle fighting" role, but the Army's broader concern was the task of protecting Western Europe from the legions of Warsaw Pact armor to the east. The Army had initiated the Advanced Aerial Fire Support System (AAFSS) program to develop the Lockheed AH-56 Cheyenne for the anti-tank gunship role, but development of the Cheyenne did not go smoothly, and as one writer put it, "the vultures began to gather", with Sikorsky and Bell trying to sell unsolicited alternatives to the Army. The Sikorsky offering was the S-67 Blackhawk, a sleek gunship, which despite the name had no real relation to the later UH-60 Black Hawk utility transport helicopter. The Bell offering was a refined HueyCobra, the Model 309 KingCobra.

Bell announced the KingCobra program in January 1971. Two prototypes were built, one with a P&WC T400-CP-400 Twin Pac dual turboshaft engine system much like that used on the AH-1J, but with a stronger drivetrain allowing operation at full 1,800 shp (1,340 kW) power, and the other with a single Lycoming T55-L-7C turboshaft engine rated at 2,000 shp (1,490 kW). The twin-engine KingCobra first flew on 10 September 1971. It looked much like an AH-1J, except for a longer and distinctive "buzzard beak" nose and a ventral fin like that on the original Model 209 demonstrator. However, there were significant changes that were less noticeable: • The airframe was strengthened and the tailboom was lengthened, making the KingCobra 3 ft longer than the AH-1G. • A new rotor was fitted, with forward swept tips and a diameter of 48 ft, compared to 44 ft for the AH-1G. The new rotor blades improved lift and reduced noise. • A larger 20 millimeter ammunition drum, derived from the General Dynamics F-111, was fitted, which required a deeper fuselage. • A sensor system for night and bad weather fighting was fitted beneath the extended nose. This Stabilized Multisensor Sight (SMS) was derived from technology developed for the AH-56 Cheyenne, and included a FLIR, a low-light television (LLTV), a laser rangefinder, and a missile guidance system. The SMS could display imagery on either the gunner's sight or the pilot's head-up display (HUD). The pilot had his own LLTV, mounted in the front of the rotor fairing, to allow him to fly while the gunner hunted for targets. New avionics were incorporated, including a Litton inertial navigation system (INS) that could store 16 different preprogrammed navigation waypoints; a radar altimeter with a ground warning system; and other improved navigation and communications gear. The primary weapon of the KingCobra was to be the new wire-guided BGM-71 TOW anti-tank missile, which had proven highly effective in combat test firings in Vietnam from Huey gunships. This weapon could be carried in a pack of four missiles, with one pack under each stub wing for a total of eight missiles. On launch, the TOW trailed out wires to communicate command guidance updates. The missile had two infrared flares on its tail to allow the SMS to track it. All the gunner had to do was keep the target in his sight, and the missile fire control system adjusted its flight appropriately. Both the gunner and the pilot had Sperry Univac helmet-mounted sights to allow them to acquire targets for the KingCobra's missiles and gun. A long-span "big wing", 13 ft wide, was designed for the KingCobra, but apparently never fitted except as a static mockup. The "big wing" was to provide additional fuel and stores carriage capability at the wingtips.

The single-engine KingCobra first flew in January 1972. Other than engine fit, it was almost identical to the twin-engine KingCobra. As it turned out, the single-engine prototype was wrecked in an accident in April, and to complete US Army evaluation the twin-engine KingCobra was modified to the single-engine configuration. The evaluation, which pitted the KingCobra against the Lockheed Cheyenne and Sikorsky S-67 in a competitive fly-off, began in the spring of 1972 and was completed in July. In August, the Army rejected all three to everyone's surprise.

• Model 249: Experimental version fitted with four rotor blades. • Model 309 KingCobra: Experimental version powered by one Lycoming T55-L-7C engine. • Model 309 KingCobra: Experimental version powered by two engines.