PLAY
Aviation
Welkin F.Mk.I
IV
Rank
AB
4.7
RB
4.7
SB
4.7
Battle rating
Great Britain
Research country
Fighter
Main role
46,000
RP
Research
155,000
SL
Purchase
General information

Upon the arrival of German high-altitude Ju 86P bombers, the Royal Air Force (RAF) began developing a high-altitude interceptor. The Air Force was primarily concerned about the potential for renewed bombing raids on Britain from high altitudes. In 1940, Westland proposed adapting the Whirlwind fighter for this new mission. To accomplish this, they significantly increased the aircraft's wingspan and replaced its original engines with Rolls-Royce Merlins. A pressurized cockpit was also introduced.

In January 1941, the Ministry of Aircraft Production approved the construction of two Westland P.14 prototypes, pitting them against a single Vickers Type 432 prototype. The first prototype took to the skies on November 1, 1942, and the second in March 1943. The RAF deemed the fighter superior to other alternatives, designated it the Welkin, and ordered 100 F.Mk.I. aircraft. Despite entering series production, the aircraft was highly problematic. Due to the large wing thickness required for such a wingspan, the aircraft was prone to stalling or shock stall. Furthermore, the Welkin was heavy, making it useful only for intercepting high-altitude bombers. By the time the Welkin entered service in May 1944, high-altitude variants of the Spitfire were already performing this task successfully. Consequently, the Welkin was used for training in intercept tactics and never saw combat. By November, the fighter had been withdrawn from frontline units, and production halted at 77 aircraft, including prototypes.

The Welkin F.Mk.I was introduced Update 2.57 "Heavy Cavalry". It is a fighter with powerful offensive armament, good vertical maneuverability, and generally good performance at high altitudes. However, it has a low top speed and poor roll rate.



Flight performance
Max speed
at 8,000 m 659613687630 km/h
Rate of Climb 17.312.72312.7 m/s
Turn time 18.720.61819.9 s
Max altitude 12,000 m
Takeoff Run 650 m

Landing
flaps
Take-off
flaps
Combat
flaps
Air
brake
General characteristics
Crew 1 person
Engine
Length 12.6 m
Wingspan 21.3 m
Wing Loading 208 kg/m²

Weight:
Base weight 7.017.236.837.2 t
Fuel in main tanks 1.89 t (2h 14m)

Limits:
Max Speed Limit (IAS) 675 km/h
Mach Number Limit 0.8 M
G limit ≈ -4/7 G
Flap Speed Limit (IAS) L / T
270 / 341 km/h
Gear Speed Limit (IAS) 320 km/h
Offensive armament
4 × 20 mm Hispano Mk.II cannon
Ammunition 566 rounds
Fire rate 600 shots/min
One-second Burst Mass 1.32 kg

BeltBelt fillingArmor penetration (mm) at a distance:
10 m100 m500 m1000 m1500 m2000 m
HEI/SAP-I/T222014964
AP-T/HEI/SAP-I37352516107
T/HEI/SAP-I/HEI/SAP-I222014964
AP-T/T/HEI37352516107
AP-T/SAP-I/HEI/AP-T37352516107
HEI/HEI/SAP-I222014964
Economy
Repair cost Basic → Reference
AB 1,863 → 2,549 SL
RB 4,359 → 5,963 SL
SB 6,089 → 8,330 SL
Crew training 45,000 SL
Experts 155,000 SL
Aces 820 GE
Research Aces 440,000 RP
Reward multiplier AB / RB / SB
80 / 200 / 410 % SL
160 % RP
Total cost of modifications 40,500 RP
78,200 SL
Talisman cost 1,400 GE

Research order:

Flight performance
Survivability
Weaponry
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