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Su-30 Flanker-C vs Su-33 Flanker-D

Su-30 Flanker-C vs Su-33 Flanker-D at a glance — top speed 2,125 vs 2,300 km/h, range 3,000 vs 3,000 km, max takeoff weight 34,500 vs 33,000 kg, built 630 vs 22 units.

Specifications
Su-30 Flanker-C Su-33 Flanker-D
Origin country 🇷🇺 Ex-USSR 🇷🇺 Ex-USSR
Category Combat Aircraft Combat Aircraft
Manufacturer Sukhoi Sukhoi
First flight 30 December 1989 17 August 1987
Year introduced 1996 1998
Number produced 630 units 22 units
Average unit price $37 million $45 million
Wing area 62.0 m² -- m²
Wingspan 14.7 m 15.0 m
Height 6.4 m 6.0 m
Length 21.9 m 22.0 m
Maximum speed 2125 km/h 2300 km/h
Operational range 3,000 km 3,000 km
Service ceiling 17,500 m 18,000 m
Max. takeoff weight 34,500 kg 33,000 kg
Empty weight 17,700 kg 14,800 kg
Total thrust 2 x 12,500 kgf 2 x 12,797 kgf
Performance Radar Chart

Detailed Comparison

Sukhoi’s Su-30 and Su-33 evolved from the baseline T-10 airframe to satisfy opposing doctrinal requirements. The Su-30 emerged as a two-seat, land-based multirole strike fighter that captured the global export market with 630 units built. The Su-33 was strictly engineered as a fleet air defense interceptor for the Soviet Navy’s Project 1143.5 carrier, yielding a total production run of just 22 airframes before the line closed.

Development and Design

The Su-33 prioritized STOBAR (Short Take-Off But Arrested Recovery) operations for the Admiral Kuznetsov. Sukhoi integrated canards to increase low-speed lift, reinforced the undercarriage, and added an arrestor hook and folding wings to reduce deck footprint. The Su-30 went in a different direction, adding a second seat for a Weapons System Officer (WSO) to manage air-to-ground ordnance and long-range radar tasks. Later variants of the Su-30, particularly the Indian Su-30MKI and Russian Su-30SM, incorporated canards and AL-31FP thrust-vectoring nozzles to regain the dogfighting agility lost to the heavier 17,700 kg two-seat airframe.

Specifications and Performances

A comparison of the airframes reveals the aerodynamic and operational tolls of navalization. The Su-33 achieves a higher maximum speed of 2,300 km/h compared to the Su-30’s 2,125 km/h, largely because early Su-30 variants carry a drag-inducing twin-seat canopy. However, the Su-33 suffers from strict payload limits. Operating from a ski-jump mandates lower takeoff weights, meaning Su-33s rarely launch with their theoretical 33,000 kg maximum takeoff weight or full internal fuel.

The land-based Su-30 faces no such restrictions. Using its full MTOW, the aircraft routinely carries heavier ordnance profiles:

  • Heavy anti-ship and standoff missiles (Kh-31, Kh-59)
  • Active radar homing air-to-air missiles (R-77)
  • Western and indigenous targeting pods (on export variants)

Both share a 3,000 km baseline range, but the Su-30's dual-crew layout makes long-duration missions practically executable.

Deployment and usage

The Su-30 operates globally. The Indian Air Force flies over 260 Su-30MKIs, employing them during the 2019 Balakot skirmishes for combat air patrol against Pakistani F-16s. Russian Su-30SMs routinely conduct strike and escort missions in Ukraine and Syria. By contrast, the Su-33 remains an operational dead end. Its sole combat deployment occurred off the Admiral Kuznetsov in Syria in 2016. Operations were curtailed after a Su-33 was lost to an arresting wire failure. The Russian Navy has since shifted procurement to the lighter MiG-29K, recognizing the Su-33 lacks modern precision-guided munitions capability and modern radar integration.

Conclusion

The Su-30 possesses a definitive edge in utility, combat effectiveness, and survivability. Sukhoi successfully evolved the land-based Flanker into a modernized strike platform capable of integrating standoff weapons and thrust-vectoring evasion tactics. The Su-33 is an obsolete maritime interceptor constrained by its carrier’s lack of catapults, an exorbitant $45 million unit cost, and its own 1990s-era analog avionics. For any operator requiring multirole mass and modern sensor integration, the Su-30 is the sole viable option.

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Frequently Asked Questions

Which is faster, the Su-30 Flanker-C or Su-33 Flanker-D?
The Su-33 Flanker-D is faster with a maximum speed of 2,300 km/h compared to the Su-30 Flanker-C's 2,125 km/h, a difference of 175 km/h.
Which has longer range, the Su-30 Flanker-C or Su-33 Flanker-D?
Both the Su-30 Flanker-C and Su-33 Flanker-D have a range of 3,000 km.
Which can fly higher, the Su-30 Flanker-C or Su-33 Flanker-D?
The Su-33 Flanker-D has a higher service ceiling at 18,000 meters (59,055 ft) compared to the Su-30 Flanker-C's 17,500 meters (57,414 ft).
Which is heavier, the Su-30 Flanker-C or Su-33 Flanker-D?
The Su-30 Flanker-C has a higher maximum takeoff weight at 34,500 kg compared to the Su-33 Flanker-D's 33,000 kg.
Which is larger, the Su-30 Flanker-C or Su-33 Flanker-D?
The Su-33 Flanker-D is longer at 22.0 meters compared to the Su-30 Flanker-C's 21.9 meters.
Which is more expensive, the Su-30 Flanker-C or Su-33 Flanker-D?
The Su-33 Flanker-D is more expensive at approximately $45 million per unit compared to the Su-30 Flanker-C at $37 million.
Which entered service first, the Su-30 Flanker-C or Su-33 Flanker-D?
The Su-30 Flanker-C entered service first in 1996, 2 years before the Su-33 Flanker-D which entered service in 1998.
Which has been built in greater numbers, the Su-30 Flanker-C or Su-33 Flanker-D?
The Su-30 Flanker-C has been produced in greater numbers with 630 units compared to 22 units of the Su-33 Flanker-D.