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Aviation
▄F-5T SCU
VII
Rank
AB
11.7
RB
11.3
SB
11.7
AB
—
RB
11.3
SB
11.3
AB
11.7
RB
11.3
SB
—
Battle rating
Japan
Research country
Fighter
Main role
260,000
RP
Research
720,000
SL
Purchase
Thailand
Operator
General information

The F-5T SCU (Second Capability Upgrade), also known as F-5T Tigris, was the second modernisation of the American F-5E fighter-bomber by the Thai military. After retiring the F-5A and making minor modifications to the F-5E, the Thai military decided to upgrade the ageing aircraft more comprehensively. In the late 1990s, they enlisted the help of the Israeli company Elbit, which created a design for new cockpit glass, digital multifunction displays (MFDs), a helmet-mounted target designation system, a new radar, and a new rudder. Upgrades to the F-5T Tigris began in 2002, and 18 aircraft were modified. The aircraft were scheduled for decommissioning in the early 2010s; however, due to financial constraints, in 2015 it was decided to upgrade the aircraft to the TSU (Third Capability Upgrade) level, resulting in the F-5TH Super Tigris. The F-5TH is expected to remain in service until the early 2030s.

Introduced in Update "Storm Warning" as part of the Thai sub-tree, the F-5T SCU is an upgraded version of the F-5 fighters, further improving its impressive versatility with new ordnance options. Compared to the related F-5E FCU, the F-5T trades an option to carry additional all-aspect missiles in favour of carrying a pair of deadly AIM-9L all-aspect missiles with improved characteristics over the AIM-9P-4 found on the FCU. In addition, the F-5T features the addition of HMD targeting, allowing the pilot to better take aim at their target.



Flight performance
Max speed
at 11,582 m 1,7781,7421,8331,753 km/h
Rate of Climb 150117171.2130.7 m/s
Turn time 2627.824.927.2 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 14.7 m
Wingspan 8.1 m
Wing Loading 402 kg/m²

Weight:
Base weight 4.955.114.825.08 t
Fuel in main tanks 2 t (38m)
Fuel in drop tanks 1.38 t (26m)

Limits:
Max Speed Limit (IAS) 1,458 km/h
Mach Number Limit 1.75 M
G limit ≈ -5/11 G
Flap Speed Limit (IAS) L / T / C
463 / 472 / 1,203 km/h
Gear Speed Limit (IAS) 482 km/h
Offensive armament
2 × 20 mm M39A3 cannon
Ammunition 560 rounds
Fire rate 1,698 shots/min
One-second Burst Mass 2.82 kg

BeltBelt fillingArmor penetration (mm) at a distance:
10 m100 m500 m1000 m1500 m2000 m
HEF-I/HEF-I/API-T/AP-I3834201053
HEF-I/API-T/AP-I3834201053
HEF-I/HEF-I/HEF-I/API-T/AP-I3834201053
API-T/AP-I/AP-I3834201053
HEF-I/HEF-I/HEF-I/AP-I3834201053
Suspended armament
Max weight 7,257 kg
Wing loading left / right
Maximum 3,000 kg
Max. difference 1,500 kg

NameWeightSlot
84.5 kg
121 kg
19 × 233.7 kg
4 × 280.3 kg
210.5 kg
240.9 kg
401.4 kg
446.8 kg
Drop tank (150 gal.)80 kg
893.6 kg
Drop tank (150 gal.)80 kg
Economy
Repair cost Basic → Reference
AB 3,100 → 4,188 SL
RB 8,848 → 11,954 SL
SB 10,360 → 13,996 SL
Crew training 200,000 SL
Experts 720,000 SL
Aces 3,200 GE
Research Aces 1,210,000 RP
Reward multiplier AB / RB / SB
100 / 320 / 540 % SL
244 % RP
Total cost of modifications 217,800 RP
336,000 SL
Talisman cost 3,000 GE

Research order:

Flight performance
Survivability
Weaponry
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