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F-89 Scorpion




The Northrop F-89 Scorpion was an early American Jet-powered all-weather Interceptor . It has the distinction of being the first Aircraft armed with Nuclear Weapon s (the Genie missile) for air-to-air use.


DEVELOPMENT

The Scorpion stemmed from a 1945 United States Army Air Forces specification for a jet-powered Night Fighter to replace the P-61 Black Widow . Northrop submitted a proposal labeled N-24, a slim-bodied aircraft with a cantilevered mid-mounted wing and two Allison J35 Turbojet Engine s with Afterburner s. It was to have Radar and a crew of two, with an armament of six 20 mm cannon in a unique trainable nose Turret . Contracts for two Prototype s were issued in December 1946 .

The initial XP-89 prototype made its first flight on 16 August 1948 . A unique feature added to the prototype during development was the Deceleron , a two-part Aileron that could split open to act as an air brake; this feature was to become a Northrop trademark, still used today on the B-2 Spirit .

Production was authorized in January 1949 , with the first production F-89A entering USAF service in September 1950 . It had AN/APG-33 radar and an armament of six T-31 20 mm cannon with 200 rounds per gun. The swiveling nose turret was abandoned, and 300 US gallon (1,100 L) fuel tanks were permanently fitted to the wingtips. Underwing racks could carry 16 five-inch aerial rockets or up to 3,200 lb (1,455 kg) of bombs.

Only eight F-89As were completed before the type was upgraded to F-89B standard, with new avionics. These had considerable problems with engines and other systems, and soon gave way to the '''F-89C'''. Despite repeated engine changes, problems persisted, compounded by the discovery of structural problems with the wings that forced a refit of 194 -A, -B, and -C models.

The major production model was the F-89D, which first flew 23 October 1951 and entered service in 1954 . It deleted the cannon in favor of a new Hughes E-6 fire control system with AN/APG-40 radar and an AN/APA-84 computer. Armament was two pods of 52 2.75 in (70 mm) "Mighty Mouse" FFAR rockets, for a total of 104. A total of 682 were built.

Proposed re-engined F-89s, designated F-89E and '''F-89F''', were not built, nor was a proposed '''F-89G''' that would have used Hughes MA-1 fire control and GAR-1/GAR-2 Falcon Air-to-air Missile s like the F-102 Delta Dagger .

The subsequent F-89H, which entered service in 1956 , had an E-9 fire control system like that of the early F-102 and massive new wingtip pods each holding three Falcons (usually three Semi-active Radar Homing GAR-1s and three Infrared GAR-2s) and 21 FFARs, for a total of six missiles and 42 rockets. Problems with the fire control system delayed the -H's entry into service, by which time its performance was notably inferior to newer Supersonic interceptors, so it was phased out of USAF service by 1959 .

The final variant was the F-89J. This was based on the F-89D, but replaced the standard wingtip missile pod/tanks with 600-gal fuel tanks and fitted a pylon under each wing for a single MB-1 Genie nuclear rocket (sometimes supplemented by up to four conventional Falcon air-to-air missiles). The F-89J became the first aircraft to fire a live Genie on 19 July 1957 . There were no new-build F-89Js, but 350 -Ds were modified to this standard. They served with the ADC through 1959 and with the Air National Guard through 1968 .

A total of 1,050 Scorpions of all marks was produced.


OPERATORS



SPECIFICATIONS (F-89D)

  plane Or Copter plane
  jet Or Prop jet
  crew Two
  length Main 53 ft 10 in
  length Alt 164 m
  span Main 60 ft 5 in
  span Alt 184 m
  height Main 17 ft 6 in
  height Alt 53 m
  area Main 606 ft&sup2
  area Alt 563 m&sup2
  empty Weight Main 24,200 lb
  empty Weight Alt 11,000 kg
  loaded Weight Main 42,250 lb
  loaded Weight Alt 19,200 kg
  max Takeoff Weight Main 46,800 lb
  max Takeoff Weight Alt 21,200 kg
  engine (jet) Allison J35-A-35A
  type Of Jet Turbojet s
  number Of Jets 2
  thrust Main 5,600 lbf dry, 7,400 lbf with afterburning
  thrust Alt 249 kN / 329 kN
  max Speed Main 636 mph
  max Speed Alt 1,020 km/h
  range Main 1,367 miles
  range Alt 2,200 km
  ceiling Main 49,200 ft
  ceiling Alt 15,000 m
  climb Rate Main 8,360 ft/min
  climb Rate Alt 425 m/s
  loading Main 697 lb/ft&sup2
  loading Alt 3404 kg/m&sup2
  thrust/weight 035




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