Скачать с ютуб F-101 Voodoo | Supersonic Nuclear Armed Fighter Bomber And Photo Reconnaissance Aircraft в хорошем качестве

F-101 Voodoo | Supersonic Nuclear Armed Fighter Bomber And Photo Reconnaissance Aircraft

The McDonnell F-101 Voodoo is a supersonic jet fighter which served the United States Air Force (USAF) and the Royal Canadian Air Force (RCAF). Initially designed by McDonnell Aircraft Corporation as a long-range bomber escort (known as a penetration fighter) for the USAF's Strategic Air Command (SAC), the Voodoo was instead developed as a nuclear-armed fighter-bomber for the USAF's Tactical Air Command (TAC), and as a photo reconnaissance aircraft based on the same airframe. An F-101A set a number of world speed records for jet-powered aircraft, including fastest airspeed, attaining 1,207.6 miles (1,943.4 km) per hour on 12 December 1957. They operated in the reconnaissance role until 1979. Delays in the 1954 interceptor project led to demands for an interim interceptor aircraft design, a role that was eventually won by the B model of the Voodoo. This required extensive modifications to add a large radar to the nose of the aircraft, a second crew member to operate it, and a new weapons bay using a rotating door that kept its four AIM-4 Falcon missiles or two AIR-2 Genie rockets hidden within the airframe until it was time to be fired. The F-101B entered service with USAF Air Defense Command in 1959 and the Royal Canadian Air Force in 1961. US examples were handed off to the USAF Air National Guard where they served until 1982. Canadian examples remained in service until 1984. The Voodoo's career as a fighter-bomber was relatively brief, but the reconnaissance versions served for some time. Along with the US Air Force's Lockheed U-2 and US Navy's Vought RF-8 Crusaders, the RF-101 reconnaissance variant of the Voodoo was instrumental during the Cuban Missile Crisis and saw extensive service during the Vietnam War. Interceptor versions served with the Air National Guard until 1982, and in Canadian service, they were a front line part of NORAD until their replacement with the CF-18 Hornet in the 1980s. While the Voodoo was a moderate success, it may have been more important as an evolutionary step towards its replacement in most roles, the F-4 Phantom II, one of the most successful Western fighter designs of the 1950s. The Phantom would retain the twin engines, twin crew for interception duties, and a tail mounted well above and behind the jet exhaust but was an evolution of the F3H Demon while the Voodoo was developed from the earlier XF-88 Voodoo. Initial design on what would eventually become the Voodoo began just after World War II in response to a USAAF Penetration Fighter Competition in 1946. This called for a long-range, high-performance fighter to escort a new generation of bombers, much as the North American P-51 Mustang had escorted the Boeing B-17 Flying Fortresses and Consolidated B-24 Liberators in World War II. Several companies responded with designs, and the Air Force provided funds for several of them to produce prototypes. After being awarded a contract (AC-14582) on 14 February 1947, McDonnell built two prototypes, designated the XF-88 Voodoo. The first prototype (serial number 46-6525), powered by two 3,000 lbf (13.3 kN) Westinghouse XJ34-WE-13 turbojets, flew from Muroc on 20 October 1948. Preliminary testing revealed that while handling and range was adequate, the top speed was a disappointing 641 mph (1,032 km/h) at sea level. After fitting McDonnell-designed afterburners to the second prototype, thrust was increased to 3,600 lbf (16.1 kN) with corresponding performance increases in top speed, initial rate of climb and reduced takeoff distance. Fuel consumption was greatly increased by use of the afterburners, however, reducing the range. General characteristics Crew: 2 Length: 67 ft 5 in (20.55 m) Wingspan: 39 ft 8 in (12.09 m) Height: 18 ft 0 in (5.49 m) Wing area: 368 sq ft (34.2 m2) Airfoil: root: NACA 65A007 (modified); tip: NACA 65A006 (modified)[43] Empty weight: 28,495 lb (12,925 kg) Gross weight: 45,665 lb (20,713 kg) Max takeoff weight: 52,400 lb (23,768 kg) Fuel capacity: 2,053 US gal (1,709 imp gal; 7,770 l) internals plus 2x optional 450 US gal (370 imp gal; 1,700 l) drop-tanks Powerplant: 2 × Pratt & Whitney J57-P-55 afterburning turbojet engines, 11,990 lbf (53.3 kN) thrust each dry, 16,900 lbf (75 kN) with afterburner Performance Maximum speed: 1,134 mph (1,825 km/h, 985 kn) at 35,000 ft (11,000 m) Maximum speed: Mach 1.72 Range: 1,520 mi (2,450 km, 1,320 nmi) Service ceiling: 58,400 ft (17,800 m) Wing loading: 124 lb/sq ft (610 kg/m2) Thrust/weight: 0.74 Armament Missiles: 4 (originally 6)× AIM-4 Falcon, or 2× AIR-2 Genie nuclear rockets, plus 2× AIM-4 Falcon Avionics Hughes MG-13 fire control system #voodoo #F101 #aircraft