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Northrop F-89 Scorpion

All-Weather Interceptor Aircraft

Northrop F-89 Scorpion

All-Weather Interceptor Aircraft

OVERVIEW
SPECIFICATIONS
ARMAMENT
VARIANTS
HISTORY
MEDIA
OVERVIEW



The Northrop F-89 Scorpion jet-powered interceptor provided a decade of Cold War air defense for North America.
National Flag Graphic
ORIGIN: United States
YEAR: 1950
MANUFACTURER(S): Northrop Aviation Corporation - USA
PRODUCTION: 1,050
OPERATORS: United States
SPECIFICATIONS



Unless otherwise noted the presented statistics below pertain to the Northrop F-89D Scorpion model. Common measurements, and their respective conversions, are shown when possible.
CREW: 2
LENGTH: 53.84 feet (16.41 meters)
WIDTH: 59.65 feet (18.18 meters)
HEIGHT: 17.59 feet (5.36 meters)
WEIGHT (EMPTY): 25,194 pounds (11,428 kilograms)
WEIGHT (MTOW): 42,241 pounds (19,160 kilograms)
ENGINE: 2 x Allison J-35-A-35 turbojet engines with afterburner developing 7,200 lb of thrust.
SPEED (MAX): 636 miles-per-hour (1024 kilometers-per-hour; 553 knots)
RANGE: 2,600 miles (4,184 kilometers; 2,259 nautical miles)
CEILING: 49,196 feet (14,995 meters; 9.32 miles)
RATE-OF-CLIMB: 5,250 feet-per-minute (1,600 meters-per-minute)




ARMAMENT



ORIGINAL:
6 x 20mm T-31 internal cannons

STANDARD:
104 x "Mighty Mouse" 2.75-inch air-to-surface rockets in wingtip launchers.

OPTIONAL:

3 x Falcon air-to-air missiles
27 x Mighty Mouse 70mm unguided rockets
VARIANTS



Series Model Variants
• XF-89 - Initial prototype; fitted with Allison J-35-A-9 series engines of 4,000lbs thrust.
• XF-89A - Second prototype with J-35-A-21A engine of 5,100lbs thrust; 6 x 20mm internal cannons added.
• F-89A - Initial production variant; evaluation models numbering eight total examples; modified tailplanes.
• F-89B - Second production mark; upgraded avionics suite; 40 examples produced, limited by engine issues.
• F-89C - Third production mark; fitted with J-35-A-21 / -33 series engines of 5,600lbs thrust; production limited to 164 examples.
• YF-89D - F-89B production model with new avionics and armament package.
• F-89D - Definitive F-89 mark based on YF-89D prototype; sans 6 x 20mm internal cannons; wingpods fitting 104 x rockets; Hughes E-6 fire control system; AN/APG-40 series radar coupled to AN/APA-84 computer system; 682 examples produced.
• YF-89E - Developmental testbed from F-89C production model for Allison YJ71-A-3 engine of 7,000lbs thrust.
• F-89F - Proposed variant fitting J71 engine with new fuselage design and wing assemblies; not selected for serial production.
• F-89G - Proposed improved F-89 with Hughes MA-1 fire control system with support for GAR-1/-2 Falcon air-to-air missiles.
• YF-89H - Three F-89D converted testbed airframes.
• F-89H - Fitted with E-9 fire control system; support for 6 x GAR-1/-2 Falcon air-to-air missiles with 42 x FFAR; 156 examples produced.
• F-89J - Final F-89 variant; F-89D conversions with support for 2 x MB-1 Genie nuclear rockets with 4 x Falcon air-to-air missiles; 350 conversions from F-89D production models.
• DF-89A - F-89A production models modified as aerial drones.
• DF-89B - F-89B production models modified as aerial drones.


HISTORY



Detailing the development and operational history of the Northrop F-89 Scorpion All-Weather Interceptor Aircraft.  Entry last updated on 8/18/2016. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
The Northrop F-89 Scorpion delivered a decade of service to the United States Air Force, charged with the critical defense of the upper North of the American continent from Soviet bomber incursions during the Cold War. The design was a relatively large two-seat, jet-powered fighter-type interceptor aircraft specifically designed to a USAF specification intended to replace the outgoing, propeller-driven Northrop F-61 "Black Widow" and North American F-82 "Twin Mustang" aircraft with origins in World War 2. The USAF commissioned work on the program in 1945 which resulted in a first flight of the XP-89 prototype on August 16th, 1948. The F-89 Scorpion was officially introduced in September of 1950 as the newest USAF dedicated interceptor.

The F-89, itself, was largely conventional for the time, arranged with an internal twin-engine turbojet configuration and air intakes mounted low along the fuselage sides. The engines exhausted from individual ports under and behind each wing root at the base of the empennage. One of the more novel design features was use of the "deceleron" control surface which was utilized as a "speedbrake" for lining up behind potential targets prior to firing. The aircraft was managed by two crewmembers - the pilot in the forward cockpit with the radar operator in the rear. The elongated nose cone assembly housed a powerful radar system that would be utilized for the required interception sorties. The wings were straight assemblies fitted at amidships and (eventually) capped with wingtip-mounted unguided rocket pods in streamlined nacelles (up to 104 x "Mighty Mouse" rockets were housed altogether). Additionally, later Scorpion models could be outfitted with a combination load of Falcon air-to-air missiles and Mighty Mouse rockets - all intended to bring down large enemy bombers. While not granted exceptional performance benefits in her design (no thanks to the use of straight wings lacking any sweep), the F-89 was gifted with a service ceiling that allowed the system to avoid potentially lethal low-altitude confrontations with ground-launched missiles or enemy interceptors. When at rest, the F-89 certainly promoted a very distinct low-set profile, its fuselage belly nearly skirting the turf. The undercarriage was wholly retractable and consisted of two single-wheeled main legs under the wings and a single-wheeled nose leg under and ahead of the cockpit floor.

internally, and the main reason for the aircraft's existence and success, the ultimate form of the F-89 was equipped with the then-powerful AN/APG-40 series radar suite coupled to the AN/APA-84 computer system capable of tracking aerial targets up to 50 miles out. The system was tied to the technologically-laden Hughes fire control system (FCS) which featured an integrated advanced autopilot function. All told, the collective system was designed to be able to track targets, guide the aircraft to within range of the onboard armament and automatically engage targets without pilot input.

The F-89 series served the USAF primarily throughout the tumultuous 1950s in a frontline capacity before being relegated to second line duty the decade following. All F-89 versions were then out of service by the end of the 1960s after some 1,050 examples had been delivered. At the time of its inception, the F-89 marked two "firsts" becoming the first operational combat-level aircraft outfitted with nuclear-tipped air-to-air weaponry (in the Genie rocket) and the first USAF jet-powered fighter to support guided munitions. Ex-USAF mounts were transferred to the Air National Guard for the remainder of her days. The last F-89 was retired from ANG service in July 1969.




Northrop F-89 Scorpion (Cont'd)

All-Weather Interceptor Aircraft

Northrop F-89 Scorpion (Cont'd)

All-Weather Interceptor Aircraft



Operational production variants were preceded by the original XF-89 prototype (2 x Allison J-35-A-9 engines of 4,000lbs thrust each) which was followed by the XF-89A prototype (J-35-A-21A engine of 5,100lbs thrust each - 6,800lbs thrust with afterburner). The initial production model (essentially operational evaluation mounts) became the F-89A of which only eight were produced and these were slightly different from the prototypes in that their tailplanes were modified. Additionally, these production models fitted 6 x cannons as base armament. The F-89B was the second production airframe which incorporated an improved avionics package and 40 of the type were produced by Northrop, eventually dogged (and ultimately limited) by engine issues. These were naturally followed into service by the improved F-89C with their 2 x J-35-A-21/-33 series engines of 5,600lb/7,400lb thrust each. however, wing integrity issues eventually plagued all three of these early marks which limited them in many ways - especially production numbers.

The definitive production mark of the Scorpion line became the F-89D (born of a modified F-89B as the "YF-89D") which did away with the onboard internal cannon arrangement and brought about use of wingtip rocket launchers instead. The type was further advanced by the installation of the Hughes E-6 FCS, AN/APG-40 radar with AN/APA-84 series computer. The F-89D was produced in 682 examples, far outweighing all previous marks in the series by numbers alone. The F-89 enjoyed a listed maximum speed of 635 miles per hour with an ferry range of 1,360 miles. It could hit service ceilings of near-50,000 feet altitude and rise to intercept at 7,440 feet per second on full afterburner thrust. Overall bomb load was limited to 3,200lbs of externally held ordnance.

The F-89D was then followed by the F-89H of which 156 were produced (developed from three F-89D modified models under the "YF-89H" designation). These incorporated the E-9 fire control system with support for 6 x GAR-1/-2 Falcon semi-active homing/infrared (respectively) air-to-air missiles along with 42 x FFAR (Folding-Fin Aerial Rockets).

Some 350 F-89D models were later converted to the "F-89J" standard (Project Ding Dong) which utilized several underwing stations for 2 x MB-1 Genie nuclear-tipped air-to-air rockets alongside 4 x Falcon air-to-air missiles. Fuel pods or rocket pods could also be carried along the wingtip mounts as normal. During "Operation Plumb Bob" over Nevada on July 19th, 1957, the F-89J became the first aircraft to ever fire and detonate a nuclear-tipped rocket.

The "DF-89A" designation was given to ex-F-89A airframes converted to drones. Similarly, "DF-89D" drones were based on the F-89B production mark.

The F-89 was proposed or trialed in several other forms prior to its end days. The YF-89E served as a single prototype (a converted F-89C production model) for the Allison YJ71-A-3 engine of 7,000lb dry and 9,500lb afterburner engine. The F-89G was a proposed variant to be finished with the Hughes MA-1 fire control system and support for GAR-1/GAR-2 Falcon air-to-air missiles. The F-89F, another proposal, was given an all-new fuselage and wing design while incorporating the J71 series turbojet engine - alas, this mark was also not selected for serial production.

In the end, the F-89 proved a viable dedicated bomber interceptor and established a presence as a potent deterrent while providing technological stepping stone to future like-minded interceptor designs to follow. Its incorporation of an integrated autopilot system with tracking and targeting radar along with automatic weapon function would usher in a new age of interceptors that, in turn, would lead to all-new, more technologically evolved designs.




MEDIA









Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.

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Relative Maximum Speed Rating
Hi: 750mph
Lo: 375mph
    This entry's maximum listed speed (636mph).

    Graph average of 562.5 miles-per-hour.
City-to-City Ranges
NYC
 
  LDN
LDN
 
  PAR
PAR
 
  BER
BER
 
  MSK
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  TKY
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  SYD
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  LAX
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  NYC
Graph showcases the Northrop F-89D Scorpion's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
Pie graph section
Pie graph section
Pie graph section
Pie graph section
Pie graph section
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production Comparison
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units
1050
1050

  * Commercial Market High belongs to Cessna 172.

  ** Military Market High belongs to Ilyushin Il-2.


Altitude Visualization
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Supported Roles
A2A
Interception
UAV
Ground Attack
CAS
Training
ASW
Anti-Ship
AEW
MEDEVAC
EW
Maritime/Navy
SAR
Aerial Tanker
Utility/Transport
VIP
Passenger
Business
Recon
SPECOPS
X-Plane/Development
A2A=Air-to-Air; UAV=Unmanned; CAS=Close Support; ASW=Anti-Submarine; AEW=Airborne Early Warning; MEDEVAC=Medical Evac; EW=Electronic Warfare; SAR=Search-Rescue
In the Cockpit...
Supported Arsenal
Graphical image of an air-to-air missile weapon
Graphical image of a short-range air-to-air missile
Graphical image of an aircrat automatic cannon
Graphical image of an aircraft air-to-surface missile
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Commitments / Honors
Military lapel ribbon for Operation Allied Force
Military lapel ribbon for the Arab-Israeli War
Military lapel ribbon for the Battle of Britain
Military lapel ribbon for the Battle of Midway
Military lapel ribbon for the Berlin Airlift
Military lapel ribbon for the Chaco War
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Military lapel ribbon for the French-Indochina War
Military lapel ribbon for the Golden Age of Flight
Military lapel ribbon for the 1991 Gulf War
Military lapel ribbon for the Indo-Pak Wars
Military lapel ribbon for the Iran-Iraq War
Military lapel ribbon for the Korean War
Military lapel ribbon for the 1982 Lebanon War
Military lapel ribbon for the Malayan Emergency
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Military lapel ribbon for the Soviet-Afghan War
Military lapel ribbon for the Spanish Civil War
Military lapel ribbon for the Suez Crisis
Military lapel ribbon for the Vietnam War
Military lapel ribbon for Warsaw Pact of the Cold War-era
Military lapel ribbon for the WASP (WW2)
Military lapel ribbon for the World War 1
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* Ribbons not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective campaigns/operations.