PLAY
Aviation
Harrier T.10
VII
Rank
AB
11.3
RB
11.3
SB
11.3
AB
RB
11.7
SB
11.7
AB
11.3
RB
11.3
SB
Battle rating
Great Britain
Research country
Strike aircraft
Main role
Premium vehicle
Status
General information

With the arrival of the new Harrier GR.7, the RAF deemed the previous generation's two-seater Harrier T.Mk.4 and T.Mk.6 training aircraft sufficient for pilot training. The old aircraft were upgraded by installing GR.7 equipment in the nose, despite other balancing and engine power issues. However, they soon had to follow the lead of the United States Marine Corps (USMC). Initially, the USMC thought the same, but after numerous pilot training failures and inadequate preparation, they created the two-seater TAV-8B. The same problems were faced by the British, so the Air Force ordered the creation of a modification similar to the American one, but without cutting combat capabilities, with avionics and components from the GR.7. On February 28, 1990, the contract for the construction of 13 aircraft was signed.

The first two-seater Harrier T.10 took to the skies on April 7, 1994. Delivery to units began on March 1, 1995. Due to various changes, the T.10 ended up being about 90 cm longer. Only one switch was changed in the front cockpit; the second cockpit was filled with various MFDs and equipment for the pilot instructor. Despite its trainer status, the T.10 served in combat units. Like other Harriers, the T.10 was removed from RAF service by 2011.

The Harrier T.10 was introduced in Update 2.45 "Hornet's Sting". The aircraft resembles the Harrier GR.7 in many ways, differing only in the absence of the AIM-9M air-to-air missile and its inferior flight characteristics. While T.10 pilots will appreciate its vast array of countermeasures and wide range of drop weapons, its low maximum speed makes it difficult to engage in air combat or evade enemy missiles.



Flight performance
Max speed
at 0 m 1,1251,1101,1331,116 km/h
Rate of Climb 9072.111072.1 m/s
Turn time 3031.72931 s
Max altitude 12,192 m
Takeoff Run 550 m

Landing
flaps
Take-off
flaps
Combat
flaps
Air
brake
General characteristics
Crew 2 persons
Engine
Length 14.1 m
Wingspan 9.3 m
Wing Loading 490 kg/m²

Weight:
Base weight 7.077.296.897.25 t
Fuel in main tanks 3.52 t (45m)

Limits:
Max Speed Limit (IAS) 1,137 km/h
Mach Number Limit 1.1 M
G limit ≈ -4/11 G
Flap Speed Limit (IAS) L / T
556 / 829 km/h
Gear Speed Limit (IAS) 648 km/h
Suspended armament
Max weight 4,200 kg
Wing loading left / right
Maximum 1,900 kg
Max. difference 1,400 kg

NameWeightSlot
84.5 kg
19 × 263.9 kg
18 × 183.9 kg
213.1 kg
295 kg
277.1 kg
216 × Large caliber chaff countermeasures216.1 kg
226.8 kg
303.5 kg
291.2 kg
486 kg
486 kg
546.5 kg
160 × Сountermeasures (BOL)39.4 kg
160 × Сountermeasures (BOL)
123.9 kg
1,079.6 kg
151.9 kg
TIALD targeting pod120 kg
Economy
Repair cost
AB 2,245 SL
RB 5,627 SL
SB 7,751 SL
Crew training 10,000 SL
Experts 1,560,000 SL
Aces 3,200 GE
Research Aces 2,420,000 RP
Reward multiplier AB / RB / SB
2 x (85 / 340 / 600) % SL
2 x 244 % RP
Premium vehicle
All modifications are unlocked

Flight performance
Survivability
Weaponry
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Settings
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