A-5 Vigilante Article Index for
A-5
Website Links For
Vigilante
 

Information About

A-5 Vigilante




The North American A3J/A-5 Vigilante was a powerful, highly advanced carrier-based supersonic Bomber designed for the US Navy . Although its service in the strike role was very short, it saw extensive service in the Reconnaissance role.


DEVELOPMENT

In 1953 North American Aviation began a private study for a Carrier-based , long-range, all-weather strike Bomber , capable of delivering Nuclear Weapon s at supersonic speeds. This proposal, the NAGPAW (North American General Purpose Attack Weapon) concept, was accepted by the US Navy , with some revisions, in 1955 . A contract was awarded on 29 August 1956 . Its first flight occurred two years later on 31 August 1958 . Designated '''A3J-1''', the Vigilante first entered squadron service with VAH-3 in June 1961 , replacing the A-3 Skywarrior in the heavy attack role.

Under the Tri-Services Designation plan implemented under Robert McNamara in September 1962 , the Vigilante was redesignated A-5, with the initial A3J-1 becoming '''A-5A''' and the updated A3J-2 becoming '''A-5B'''. The subsequent recce version, originally '''AJ3-3P''', became the '''RA-5C'''.

The Vigilante's early service proved troublesome, with many teething problems for its advanced systems. It also arrived in service during a major policy shift in the Navy strategic role, which switched to emphasize Submarine Launched Ballistic Missile s rather than manned bombers. As a result, in 1963 procurement of the A-5 was ended and the type was converted to the fast reconnaissance role. The first RA-5Cs were delivered in July 1963, with Vigilante squadrons redesignated RVAH.

The RA-5C Vigilante saw extensive service in Vietnam starting in August 1964 , carrying out hazardous medium-level reconnaissance missions. Although it proved fast and agile, 18 were lost in combat, most to anti-aircraft fire. Several more were lost in operational accidents. 36 additional aircraft were built from 1968-1970 as attrition replacements.

Despite the Vigilante's useful service, it was expensive and complex to operate, and it was phased out after the end of the Vietnam War . Disestablishment of RVAH squadrons began in 1974 , with the last Vigilantes completing their final deployment in September 1979 .


DESCRIPTION

At the time of its introduction, the Vigilante was one of the largest and by far the most complex aircraft to operate from a US Navy Aircraft Carrier . It had a high-mounted Swept Wing with a boundary-layer Control System (blown Flaps) to improve low-speed lift, two widely-spaced General Electric J79 Turbojet Engine s (the same as used on the F-4 Phantom II ), and a single large vertical tailfin. The wings, the tail, and the nose Radome folded for carrier stowage. The Vigilante had a crew of two seated in tandem, a pilot and a bombardier-navigator (BN) — reconnaissance/attack navigator (RAN) on later Recon versions in individual Ejection Seat s.

With a clean airframe and powerful engines, the Vigilante was fast at high altitudes, although its high landing speed made returning to the carrier a challenge for inexperienced or unwary pilots. It was surprisingly agile for such a big and heavy aircraft.

The Vigilante had extremely advanced and complex electronics. It had one of the first Fly-by-wire systems of an operational aircraft (with mechanical/hydraulic backup) and a computerized AN/ASB-12 nav/attack system incorporating a Heads-up Display (one of the first), multi-mode Radar , Inertial Navigation , closed-circuit Television camera under the nose, and an early Digital Computer known as '''VERDAN''' (Versatile Digital Analyzer) to run it all. Although this system was highly sophisticated, the technology was in its infancy, and its reliability was poor. In early squadron service the system's MTBF (Mean Time Between Failures) was only 15 minutes! Although some bugs were worked out, the aircraft remained a maintenance nightmare throughout its career.

The Vigilante originally had two wing pylons, mostly intended for the carriage of Drop Tank s. Its main armament was carried in a so-called linear bomb bay, a cylindrical bay between the engines in the rear fuselage that carried a "stores train" with two disposable fuel tanks and a single Nuclear Weapon , commonly the Mk 28 bomb. The idea was for the fuel tanks to be emptied during flight to the target and then jettisoned along with the bomb by an explosive drogue gun. In practice the system was never reliable and was often dangerous. The stores train sometimes dropped out during catapult launches, dumping fuel and sometimes a live nuclear weapon on the deck, and it was prone to 'trailing' behind the Aircraft in flight, ruining any semblance of accuracy. Even later in the Vigilante's career, when the bay was used solely for fuel, it often proved troublesome.

The second Vigilante mark, the A3J-2 ('''A-5B''') added blown flaps on the leading edge of the wing, heavier Landing Gear , and a pronounced dorsal "hump" incorporating tanks for an additional 460 gallons of fuel. Two additional wing hardpoints were added, for a total of four, although in practice they were rarely used.

The Reconnaissance version of the Vigilante, the RA-5C, had slightly greater wing area and added a long canoe-shaped fairing under the fuselage for a multi-sensor reconnaissance pack. This added an '''APD-7''' side-looking airborne radar ( SLAR ), '''AAS-21''' Infrared linescanner, and camera packs, as well as improved ECM. An '''AN/ALQ-61''' electronic intelligence system could also be carried. The RA-5C retained the AN/ASB-12 bombing system, and could, in theory, carry weapons, although it never did in service. Later-build RA-5Cs had more powerful -10 engines with afterburning thrust of 17,900 lbf (80 kN). The reconnaissance Vigilante weighed almost five tons more than the strike version with almost the same thrust and an only modestly enlarged wing. These changes cost it acceleration and climb rate, though it remained fast in level flight.

Although the Vigilante served in the attack and recce roles, its design and configuration was believed to be a major influence on one of the world's most famous postwar MiG-25 'Foxbat' was apparently heavily influenced by the A-5's design. (The MiG-25 would look even more familiar if the Vigilante had retained the twin vertical fins of the prototype; although North American originally specified two fins, like the later Foxbat, that part of the design was vetoed by the Navy in favor of one folding tailfin.)


PRODUCTION

  • YA3J-1 : Prototypes, two built.

  • A3J-1 ('''A-5A'''): 59

  • A3J-2 ('''A-5B'''): 6

  • A3J-3P ('''RA-5C'''): Reconnaissance version. 91 new-build plus 43 converted A-5As



OPERATORS



SPECIFICATIONS (A3J-1/A-5A VIGILANTE)


  jet Or Prop jet
  plane Or Copter plane
  crew Two
  length Alt 2332 m
  length Main 76 ft 6 in
  span Alt 1615 m
  span Main 53 ft 0 in
  height Alt 59 m
  height Main 19 ft 5 in
  area Alt 70 m&sup2
  area Main 754 ft&sup2
  empty Weight Alt 14,846 Kg
  empty Weight Main 32,700 Lb
  loaded Weight Alt 21,579 kg
  loaded Weight Main 47,530 lb
  useful Load Alt 13,734 kg
  useful Load Main 30,250 lb
  max Takeoff Weight Alt 28,579 kg
  max Takeoff Weight Main 62,950 lb
  engine (jet) General Electric J79 -GE-8
  type Of Jet afterburning Turbojet s
  number Of Jets 2
  thrust Main 10,900 lbf
  thrust Alt 48 kN) dry (17,000 lbf (76 kN) with afterburner
  max Speed Main 20 Mach at altitude
  max Speed Alt 1,320 mph, 2,123 km/h), 10 Mach at sea level (806 mph, 1,297 km/h
  range Main 1,290 mi
  range Alt 2,075 km
  ceiling Main 52,100 ft
  ceiling Alt 15,880 m
  climb Rate Main 8,000 ft/min
  climb Rate Alt 406 m/s
  loading Main 804 lb/ft&sup2
  loading Alt 3083 kg/m&sup2
  thrust/weight 072



RECORDS AND ADDITIONAL FIRSTS

On December 13 1960 , U.S. Navy Cmdr. Leroy Heath (Pilot) and Lt. Larry Monroe (Bombardier/Navigator) established a world altitude record of 91,450.8 feet (27,874.2 metres) in an A3J Vigilante carrying a 1,000 kilogram payload, besting the previous record by over 4 miles. This new record held for over 13 years.


EXTERNAL LINKS



RELATED CONTENT