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F-16XL
Aviation

F-16XL

VIII
Rank
AB
13.3
RB
13.3
SB
13.3
AB
—
RB
13.0
SB
12.3
AB
13.3
RB
13.3
SB
—
Battle rating
USA
Research country
Fighter
Main role
General information

Following the success of the F-16, General Dynamics began exploring ways to increase the fighter jet's range and payload capacity without compromising its core strengths. In 1977, the company started working on the SCAMP (Supersonic Cruise and Maneuver Prototype) project under Harry Hillaker's leadership. One of the project's key objectives was to improve the aircraft's performance at supersonic speeds. During development, General Dynamics drew on NASA research and moved away from the original wing design of the F-16. They replaced it with a cranked-arrow wing similar to the Swedish J35's, which had a larger surface area and greater internal volume. This design allowed for larger internal fuel tanks and additional weapon hardpoints.

Subsequently, the project was designated the F-16XL, and two F-16 aircraft—an F-16A and an F-16B—were converted for testing. The first prototype made its maiden flight on July 3, 1982, followed by the two-seat prototype on October 29 of the same year. In 1981, General Dynamics proposed the F-16XL for the Enhanced Tactical Fighter program, through which the U.S. Air Force sought a replacement for the F-111. However, the McDonnell Douglas F-15E Strike Eagle was selected. Following the competition, both prototypes were placed in storage before being transferred to NASA in the late 1980s for research into supersonic flight, wing aerodynamics, and shockwave propagation.

The F-16XL was introduced as a reward for the 2026 "Space Program" event. The aircraft stands out for its large selection of suspended weapons and extended flight range. It retains the high speed, maneuverability, and other advantages of the original F-16A.


Where to purchase


Book of Records
Flight performance
Max speed
at 10,973 m 2,1562,0712,2112,102 km/h
Rate of Climb 190141.6229.8153.3 m/s
Turn time 2527.123.926.2 s
Max altitude 15,240 m
Takeoff Run 850 m

Landing
flaps
Take-off
flaps
Combat
flaps
Air
brake
General characteristics
Crew 1 person
Engine
Length 16.7 m
Wingspan 10.7 m
Wing Loading 258 kg/m²

Weight:
Base weight 8.799.088.569.03 t
Fuel in main tanks 5.11 t (1h 3m)
Fuel in drop tanks 2.27 t (28m)

Limits:
Max Speed Limit (IAS) 1,555 km/h
Mach Number Limit 2.2 M
G limit ≈ -6/12 G
Gear Speed Limit (IAS) 482 km/h
Offensive armament
20 mm M61A1 cannon
Ammunition 512 rounds
Fire rate 6,000 shots/min
One-second Burst Mass 9.98 kg

BeltBelt fillingArmor penetration (mm) at a distance:
10 m100 m500 m1000 m1500 m2000 m
HEF-I/API-T/AP-I/SAPHEI4036211163
HEF-I/HEF-I/API-T/HEF-I/HEF-I/AP-I4036211163
HEF-I/AP-I/AP-I/SAPHEI4036211163
SAPHEI3733201164
Suspended armament
Max weight 6,804 kg
Wing loading left / right
Maximum 3,000 kg
Max. difference 2,000 kg

NameWeightSlot
84.5 kg
240.9 kg
210.5 kg
893.6 kg
Drop tank (370 gal.)100 kg
4 × 963.6 kg
2 × 313 kg
4 × 626 kg
Economy
Repair cost Basic → Reference
AB 3,201 → 4,462 SL
RB 9,208 → 12,836 SL
SB 10,852 → 15,128 SL
Crew training 270,000 SL
Experts 940,000 SL
Aces 3,700 GE
Research Aces 1,380,000 RP
Reward multiplier AB / RB / SB
100 / 320 / 500 % SL
262 % RP
Total cost of modifications 301,000 RP
465,000 SL
Talisman cost 3,300 GE

Flight performance
Survivability
Weaponry
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Settings
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