Air Weapons

Lockheed

F-104 Starfighter

With a name that appealed more to science fiction than warfare, the Lockheed F-104 Starfighter was billed as 'a missile with a man in it'. Designed by a Lockheed Skunk Works team led by Clarence Johnson, the F-104 was the first operational fighter capable of Mach 2 speeds and also claimed both the world speed and altitude records. It was instantly recognizable by its slim fuselage, T-tail, and and small, mid-mounted wings which in a departure from jet aircraft convention, were designed straight rather than swept. The thin wings meant there was little room for fuel and as a result, most aircraft flew with fuel tanks fitted in the wingtips although range was still poor. The F-104 was also notable for being the first aircraft to be equipped with the M61 Vulcan cannon which would be the standard fixed armament of most US fighters since. Despite being the most ambitious of the Century Series of fighters, the F-104 was built in only small numbers for the USAF where it proved to be disappointing as both an interceptor and a fighter-bomber and it would also be haunted by a poor safety record. Its great success would lay in the export markets where most eventually served with numerous major NATO air forces in what was dubbed the 'deal of the century'. Unfortunately this too was plagued with controversy as it was later revealed that Lockheed paid millions in bribes to European politicians to obtain sales (this nearly led to Lockheed's demise). In USAF service, the Starfighter saw limited action in the Vietnam War but ultimately replaced due to the availability of superior designs for either role. Later versions were mostly geared for export and were true multi-role aircraft, significantly enhanced for air combat, ground attack, and reconnaissance missions. A total of 14 countries operated the Starfighter most of which were NATO partners (which set up production lines in Belgium, Canada, Germany, the Netherlands, and Italy) in addition to Taiwan, Japan, Jordan, and Pakistan, the latter which used it in combat against India. Some were still in service in the year 2000.

Developed from the Lockheed Model 83, the first XF-104 had its maiden flight on 4 March 1954 followed by evaluation YF-104A units and finally, the first of the F-104A units which were optimized as interceptors which could carry wingtip Sidewinder missiles. These were followed by the F-104C fighter-bombers with inflight refuelling capability and underwing hardpoints for bombs and missiles. Two-seat versions of these aircraft were known as the F-104B and D respectively while the QF-104 was a target drone conversion. The first of the multi-role variants was the F-104G intented for German service: it had a strenghtened structure, increased fuel, new avionics, and could carry air-to-air and air-to-ground weapons (most were built in Europe by a consortium that included Messerschmitt, Dornier, Fiat, Fokker, and SABCA). Related to this was the TF-104G two seater and the RF-104C reconnaissance platform. The F-104J was a similar version built by Mitsubishi for Japan but which featured only air-to-air capability. In contrast, the CF-104 built by Canadair for Canada was optimized for the strike role and initially lacked guns though they were later installed. The final Starfighter variant was the F-104S built by Fiat for Italian service. It had more powerful engines, even more weapons hardpoints, and could carry Sparrow missiles (including the Italian equivalent, the Aspide). These were further upgraded as the F-104ASA which remained in service past the turn of the century pending the introduction of the Eurofighter.

F-104A Starfighter (USAF)
F-104C

Preceded by:

None

Succeeded by:

F-5 Freedom Fighter (1962)

Datafile

DesignF-104AF-104CF-104GCF-104F-104S
NameStarfighterStarfighterStarfighterStarfighterStarfighter
TypeInterceptorFighter-BomberFighter-BomberAttackInterceptor
Year19581958196019631969
Crew11111
Dimensions
Length16.69 m16.69 m16.69 m16.69 m16.69 m
Height4.11 m4.11 m4.11 m4.11 m4.11 m
Wing Span6.63 m6.63 m6.63 m6.63 m6.63 m
Wing Area18.2 m²18.2 m²18.2 m²18.2 m²18.2 m²
Weight
Empty5,980 kg5,788 kg6,349 kg6,309 kg6,700 kg
Loaded8,159 kg8,832 kg9,362 kg9,528 kg9,839 kg
Maximum11,721 kg12,634 kg13,172 kg13,105 kg14,062 kg
Wing Loading643.4 kg/m²693.5 kg/m²723.0 kg/m²719.3 kg/m²771.8 kg/m²
Performance
SpeedMach 1.5Mach 2.3Mach 1.9Mach 2.4Mach 2.1
Speed S/L???Mach 1.2Mach 1.2
Ceiling19,751 m17,678 m15,240 m15,240 m17,678 m
Range1,175-2,253 km1,368-2,414 km1,738-2,623 km2,623 km2,921 km
Powerplant
Engine1 x J79-GE-3A/B
General Electric
4,355 / 6,713 (+) kgf
1 x J79-GE-7
General Electric
4,536 / 7,167 (+) kgf
1 x J79-GE-11
General Electric
4,536 / 7,076 (+) kgf
1 x J79-OEL-7
Orenda
4,536 / 7,167 (+) kgf
1 x J79-GE-19
General Electric
5,384 / 8,119 (+) kgf
Thrust/Weight0.660.710.650.650.73
Sensors
RadarAN/ASG-14T
AN/ASG-14T-2
F15A-41B
R-24A
R-21G
Armament
Guns1 x 20-mm
M61 (725)
1 x 20-mm
M61A1 (725)
1 x 20-mm
M61A1 (725)
-1 x 20-mm
M61A1 (725)
Payload-907 kg1,814 kg1,814 kg3,402 kg
Hardpoints45779
AA WeaponsAIM-9
AIM-9
AIM-9
-AIM-7
AIM-9
AS Weapons-B28/43
AS.30
AS.34
B43
B28/43/57
BL.755
CRV-7
-
Production
Built153771,122200246
Total2,422

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