PLAY
Aviation
▄HF-24
V
Rank
AB
8.7
RB
9.0
SB
9.0
Battle rating
Great Britain
Research country
Strike aircraft
Main role
India
Operator
General information

In the 1950s, Hindustan Aeronautics Limited (HAL) decided to enter the supersonic aviation market. At the time, HAL was producing simple training aircraft. Around this time, the Indian Air Force was looking to acquire a new fighter-bomber. The Indian government allocated funds for the aircraft's construction. Since HAL lacked experience with such technology, the company brought in Kurt Tank, known for his Fw 190 and a number of jet fighter projects. Despite the government's constantly changing requirements, a full-scale wooden model took to the skies on April 3, 1959, with the help of a Douglas Dakota transport aircraft. The new aircraft was designated the HF-24 Marut, named after the Maruts, gods of thunderstorms.

The prototype with a Bristol Siddeley Orpheus 703 engine made its first flight on June 24, 1961. However, the Orpheus proved to be a weak engine incapable of supersonic flight. The subsequent deterioration of India's relations with the West made obtaining a new, more powerful engine impossible, so all 147 aircraft were built with the Orpheus 703. Due to Kurt Tank's unwillingness to negotiate with the Indian government regarding design changes, the Air Force's lackadaisical attitude toward the project, and the inability to develop a powerful engine independently, the HF-24s were withdrawn from service by 1982. They only saw action during the third Indo-Pakistani War of 1971.

The Indian HF-24 was introduced as a reward for the 2025 "Spirit of the Tempest" event in the British air research tree. It is an aircraft with good main armament and an impressive array of weapons for attacking ground targets. However, it has three major drawbacks: it is subsonic, has poor maneuverability and lacks air-to-air missiles.


Where to purchase

Flight performance
Max speed
at 0 m 1,1341,1181,1441,124 km/h
Rate of Climb 7052.884.257.7 m/s
Turn time 2830.326.329.7 s
Max altitude 13,000 m
Takeoff Run 820 m

Landing
flaps
Take-off
flaps
Combat
flaps
Air
brake
General characteristics
Crew 1 person
Engine
Length 15.9 m
Wingspan 9 m
Wing Loading 301 kg/m²

Weight:
Base weight 6.36.516.136.47 t
Fuel in main tanks 2.02 t (26m)
Fuel in drop tanks 1.23 t (16m)

Limits:
Max Speed Limit (IAS) 1,296 km/h
Mach Number Limit 1.8 M
G limit ≈ -5/11 G
Flap Speed Limit (IAS) L / T / C
465 / 601 / 628 km/h
Gear Speed Limit (IAS) 450 km/h
Offensive armament
4 × 30 mm ADEN cannon
Ammunition 520 rounds
Fire rate 1,200 shots/min
One-second Burst Mass 5.21 kg

BeltBelt fillingArmor penetration (mm) at a distance:
10 m100 m500 m1000 m1500 m2000 m
AP/HEI-T3734221385
AP/HEI-T/AP3734221385
HEF-I/HEI-T444444
AP/HEF-I3734221385
Suspended armament
Max weight 4,100 kg
Wing loading left / right
Maximum 2,050 kg
Max. difference 1,500 kg

NameWeightSlot
4 × 114 kg
18 × 183.9 kg
235 kg
213.1 kg
486 kg
486 kg
Drop tank (100 gal.)68 kg
50 × 252.5 kg
Economy
Repair cost Basic → Reference
AB 2,611 → 3,825 SL
RB 7,267 → 10,646 SL
SB 8,808 → 12,904 SL
Crew training 98,000 SL
Experts 340,000 SL
Aces 1,800 GE
Research Aces 780,000 RP
Reward multiplier AB / RB / SB
110 / 310 / 600 % SL
202 % RP
Total cost of modifications 102,000 RP
161,200 SL
Talisman cost 2,200 GE

Flight performance
Survivability
Weaponry
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