XF-90
XF-90 in flight
General information
Type	Fighter
Manufacturer	Lockheed
Status	Canceled
Primary user	United States Air Force (Intended)
Number built	2
History
First flight	3 June 1949

TheLockheed XF-90 was built in response to aUnited States Air Force requirement for a long-rangepenetration fighter andbomber escort. The same requirement produced theMcDonnellXF-88 Voodoo. Lockheed received a contract for two prototypeXP-90s (redesignatedXF-90 in 1948). The design was developed byWillis Hawkins and theSkunk Works team underKelly Johnson. Two prototypes were built (s/n46-687 and-688). Developmental and political difficulties delayed the first flight until 3 June 1949, with Chief Test PilotTony LeVier at the controls. Embodying the experience gained in developing theP-80 Shooting Star, the XF-90 shared some design traits with the older Lockheed fighter, albeit withswept-wings; however, this latter design choice could not sufficiently make up for the project’s underpowered engines,^[1] and the XF-90 never entered production.

In response to a 1945 Army request for an advanced jet fighter, Lockheed proposed a jet powered initially by aLockheed L-1000 axial flow turbojet, and then theGeneral Electric J35.^[2] Further design refinements included using twoWestinghouse J34 engines with afterburners. After data showed that adeltaplanform would not be suitable, the Lockheed Model 90 was built in 1947 as a mock-up.^[3]

The final design embodied much of the experience and shared the intake and low-wing layout of the previousP-80 Shooting Star, but with 35°swept-back wings, a sharply-pointed nose, and twoWestinghouse J34-WE-11 axial-flow turbojet engines, providing a total thrust of 6,200 lbf (27.6 kN), mounted side-by-side in the rear fuselage and fed by side-mounted air intakes.^[1] The wings had leading edge slats, Fowler flaps, and ailerons on the trailing edge. The pressurized cockpit was fitted with an ejection seat and a bubble canopy. Proposed armament was six 20  mm (.79 in) cannons. The internal fuel was supplemented by wingtip-mounted tanks, bringing total fuel capacity to 1,665 gal (6,308 L). The use of 75ST aluminum rather than the then-standard 24ST aluminum alloy, along with heavy forgings and machined parts, resulted in a well-constructed, sturdy airframe. These innovations resulted in an aircraft with an empty weight more than 50% heavier than its competitors.^[1]

The first XF-90 used non-afterburning J34s, but these lacked the thrust for takeoff as rocket-assisted RATO were required for most of the first flights unless it carried a very low fuel load. The second (XF-90A) had afterburners installed which had been tested on anF-80 testbed. Even so, the aircraft remained underpowered.^[1]

The XF-90 was the first USAF jet with an afterburner and the first Lockheed jet to fly supersonic, albeit in a dive. It also incorporated an unusual vertical stabilizer that could be moved fore and aft for horizontal stabilizer adjustment. Partly because Lockheed's design proved underpowered, it placed second to McDonnell'sXF-88 Voodoo which won the production contract in September 1950, before the penetration fighter project was abandoned altogether.

Upon Lockheed losing the production contract, the two prototypes were retired to other testing roles. The first aircraft (46-687) was shipped to theNACA Laboratory inCleveland, Ohio in 1953 for structural tests. It was no longer flyable, and its extremely strong airframe was tested to destruction. The other (46-688) survived three atomic blasts atFrenchman Flat within theNevada Test Site in 1952.^[4]

The XF-90 lived on as the jet fighter aircraft flown by the popularBlackhawks Squadron in the comic book series of the same name, first published byQuality Comics and later byDC Comics. The Blackhawks flew fictional "B" and later "C" models all through the 1950s until 1964. Both were improved, single engine production variants of the original twin-engine Lockheed XF-90.^[5]

• 46-0687 – tested to destruction atNACA lab inCleveland, Ohio.^[6]
• 46-0688 – on display at theNational Museum of the United States Air Force inDayton, Ohio. In 2003, the heavily damaged hulk was recovered from the Nevada Test Site and moved there. Its wings have been removed, and its nose was mangled by the nuclear blasts. During the decontamination process, all rivets were removed to purge radioactive sand. The aircraft is now on display in the museum's Cold War gallery in a diorama depicting it on the Nevada Test Site.^[7][8]

General characteristics

• Crew: one
• Length: 56 ft 2 in (17.12 m)
• Wingspan: 40 ft 0 in (12.20 m)
• Height: 15 ft 9 in (4.80 m)
• Wing area: 345 sq ft (32 m²)
• Empty weight: 18,050 lb (8,204 kg)
• Gross weight: 27,200 lb (12,363 kg)
• Max takeoff weight: 31,060 lb (14,118 kg)
• Powerplant: 2 ×Westinghouse J34-WE-15turbojets, 4,100 lbf (18 kN) thrust each

Performance

• Maximum speed: 665 mph (1,064 km/h, 578 kn)
• Range: 2,300 mi (3,680 km, 2,000 nmi)
• Service ceiling: 39,000 ft (11,890 m)
• Rate of climb: 5,555 ft/min (28.2 m/s)
• Wing loading: 79 lb/sq ft (386 kg/m²)
• Thrust/weight: 0.30

Armament

• 6 × 20 mm (.79 in) cannons
• 8 × 5 in (127 mm)HVAR rockets
• Up to 2,000 lb (907 kg) of bombs

Aircraft of comparable role, configuration, and era

• McDonnell XF-88 Voodoo
• North American YF-93

Related lists

• List of Lockheed aircraft
• List of fighter aircraft
• List of military aircraft of the United States

Wikimedia Commons has media related toLockheed XF-90.

• USAF Museum: XF-90
• Operation Tumbler-Snapper: Atomic Blast Testing

• Lockheed aircraft
• 1940s United States fighter aircraft
• Twinjets
• Low-wing aircraft
• Cancelled military aircraft projects of the United States
• Aircraft with retractable tricycle landing gear

• Articles with short description
• Short description matches Wikidata
• Commons category link is on Wikidata