HAL Tejas LCA (Light Combat Aircraft) vs Airbus A380 Comparison

Aviation | Utilities | Side-by-Side Comparison

Direct side-by-side comparison of two aircraft.

Your selected aircraft are compared in side-by-side arrangement below. You can always go back and Compare any two aircraft in our database. Some entries contain '0', 'not available', or an 'NA' value. This is more common with conceptual, experimental, and x-plane designs. Rotary-wing system (i.e. helicopters) values include main rotor diameter as part of width/wingspan measurement. UAV entries may display crew values as '0', not taking into account ground-based controllers.

Subjects

HAL Tejas Mk.1
4th Generation Lightweight Multirole Fighter Aircraft

Airbus A380-800
Wide-Body, Long-Range Commercial Passenger Airliner

Basics

ORIGIN
India

ORIGIN
France

YEAR
2015 [Diff.+8 yrs]

YEAR
2007 [Diff.-8 yrs]

CREW
1

CREW
2

PRODUCTION
33 units [Diff.-217]

PRODUCTION
250 units [Diff.+217]

Dimensions

LENGTH
43.3 ft (13.2 m) [Diff.-196.2 ft]

LENGTH
239.5 ft (73.0 m) [Diff.+196.2 ft]

WIDTH/SPAN
26.9 ft (8.2 m) [Diff.-234.9 ft]

WIDTH/SPAN
261.8 ft (79.8 m) [Diff.+234.9 ft]

HEIGHT
14.4 ft (4.4 m) [Diff.-64.6 ft]

HEIGHT
79.1 ft (24.1 m) [Diff.+64.6 ft]

Relative Size Comparison

Shapes below depict aircraft from wingtip-to-wingtip / nose-to-tail assuming aircraft are being viewed from overhead perspective (the nose pointing towards the top of the screen). Helicopter widths include main rotor diameter. If any dimensional values are "NA" in the database then the presented shapes may appear skewed.

HAL Tejas Mk.1

Airbus A380-800

Weights

EMPTY WT.
14,440 lb (6,550 kg) [Diff.-595,799 lb]

EMPTY WT.
610,240 lb (276,800 kg) [Diff.+595,799 lb]

M.T.O.W.
29,762 lb (13,500 kg) [Diff.-1,204,826 lb]

M.T.O.W.
1,234,589 lb (560,000 kg) [Diff.+1,204,826 lb]

Installed Power

1 x General Electric F404-GE-IN20 afterburning turbofan engine developing 12,100lb of thrust dry and 20,200lb thrust with reheat.

4 x Engine Alliance GP7270 OR Rolls-Royce Trent 970/B turbofan engines developing between 72,000lbf to 84,000lbf of thrust each.

Performance

SPEED
1,227 mph (1,975 kph) [Diff.+593 mph]

SPEED
634 mph (1,020 kph) [Diff.-593 mph]

RANGE
1,988 miles (3,200 km) [Diff.-7,456 miles]

RANGE
9,445 miles (15,200 km) [Diff.+7,456 miles]

CEILING
54,134 ft (16,500 m) [Diff.+11,106 feet]

CEILING
43,028 ft (13,115 m) [Diff.-11,106 feet]

Armament

STANDARD:
1 x 23mm GSh-23 twin-barrel internal automatic cannon.

OPTIONAL:
Air-to-air (short-range, medium-range, and long-range), air-to-surface, laser-guided and conventional drop/launch ordnance as needed (up to 11,685lb).

External fuel replaces some weapons hardpoints.

LITENING targeting pod mounted at port side intake hardpoint.

Ordnance options also include rocket pods, anti-radiation missiles, anti-ship missiles, laser-guided bombs, Fuel-Air Explosives (FAEs), and cluster bombs.

None.

Going Further

View Entry
(HAL Tejas LCA (Light Combat Aircraft))

View Entry
(Airbus A380)

Similar

PAC JF-17 Thunder

HAL Tejas AF MWF

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