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.
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