PLAY
Aviation
F-102A
VI
Rank
AB
9.0
RB
9.0
SB
9.0
AB
—
RB
8.7
SB
8.7
AB
9.0
RB
9.0
SB
—
Battle rating
USA
Research country
Fighter
Main role
135,000
RP
Research
380,000
SL
Purchase
General information

In October 1948, the U.S. Air Force expressed interest in developing a new radar-equipped fighter interceptor. In January 1950, the military issued requirements for the radar and, in June, for the aircraft itself. Three companies were shortlisted to build the aircraft: Republic, Lockheed, and Convair. Despite its unconventional design featuring a delta wing and a missile bay, Convair's design was selected and designated the XF-102. Initially, the Curtiss-Wright J67 was considered for the interceptor's engine, but due to delays and issues with potential replacements, the designers settled for the Pratt & Whitney J57, which was less powerful. On October 23, 1953, the prototype made its first flight. A few days later, the aircraft was lost while attempting to reach supersonic speeds. The second prototype was also disappointing as it was limited to Mach 0.98.

To avoid losing such a promising contract, Convair redesigned the fighter. It was lengthened, featured new air intakes, and had a narrower cockpit. The larger, slimmer wing, a more powerful version of the J57 engine, and a lighter airframe also helped its flight performance. The redesigned YF-102A made its first flight on December 20, 1954, and broke the sound barrier the following day. The U.S. Air Force approved the fighter after the changes, and the aircraft entered mass production as the F-102A Delta Dagger. A total of 1,000 aircraft were built, some of which saw action in the Vietnam War. A few more were sold to Greece and Turkey. Due to the fighter’s mediocre flight characteristics, the F-102B variant with a J67 engine was developed; it was later designated the F-106A. The last American F-102A was withdrawn from service in 1968.

The F-102A was introduced in Update 2.59 "Sky Odyssey". This fighter is notable for its complete lack of a cannon armament; it relies entirely on infrared- and radar-guided AIM-4 missiles to shoot down enemy aircraft. However, these air-to-air missiles are difficult to use and lack a proximity fuse. Nevertheless, the aircraft may impresses with its decent speed and maneuverability.



Flight performance
Max speed
at 10,668 m 1,3821,3571,4071,364 km/h
Rate of Climb 9263.911570.5 m/s
Turn time 2628.124.527.5 s
Max altitude 13,716 m
Takeoff Run 1,050 m

Landing
flaps
Take-off
flaps
Combat
flaps
Air
brake
General characteristics
Crew 1 person
Engine
Length 14.8 m
Wingspan 11.7 m
Wing Loading 188 kg/m²

Weight:
Base weight 8.969.268.729.21 t
Fuel in main tanks 3.2 t (42m)
Fuel in drop tanks 1.26 t (16m)

Limits:
Max Speed Limit (IAS) 1,274 km/h
Mach Number Limit 1.6 M
G limit ≈ -5/11 G
Gear Speed Limit (IAS) 453 km/h
Suspended armament
Max weight 3,000 kg
Wing loading left / right
Maximum 1,000 kg
Max. difference 1,000 kg

NameWeightSlot
Drop tank (215 gal.)120 kg
66.2 kg
2 × 132.4 kg
68.9 kg
2 × 137.8 kg
12 × 107.2 kg
Economy
Repair cost Basic → Reference
AB 2,945 → 4,356 SL
RB 8,556 → 12,654 SL
SB 9,150 → 13,533 SL
Crew training 110,000 SL
Experts 380,000 SL
Aces 2,000 GE
Research Aces 830,000 RP
Reward multiplier AB / RB / SB
120 / 380 / 600 % SL
208 % RP
Total cost of modifications 114,300 RP
179,000 SL
Talisman cost 2,300 GE

Research order:

Flight performance
Survivability
Weaponry
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