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Su-27 Flanker vs Su-30 Flanker-C

Su-27 Flanker vs Su-30 Flanker-C at a glance — top speed 2,500 vs 2,125 km/h, range 3,530 vs 3,000 km, max takeoff weight 30,000 vs 33,000 kg, built 680 vs 630 units.

Sukhoi Su-27 Flanker combat aircraft side profile drawing
🇷🇺 Su-27 Flanker
Sukhoi Su-30 Flanker-C combat aircraft side profile drawing
Specifications
Su-27 Flanker Su-30 Flanker-C
Origin country 🇷🇺 Ex-USSR 🇷🇺 Ex-USSR
Category Combat Aircraft Combat Aircraft
Manufacturer Sukhoi Sukhoi
First flight 20 May 1977 30 December 1989
Year introduced 1985 1996
Number produced 680 units 630 units
Average unit price $30 million $37 million
Wing area 62.0 m² 62.0 m²
Wingspan 14.7 m 14.7 m
Height 5.9 m 6.4 m
Length 21.9 m 21.9 m
Maximum speed 2500 km/h 2125 km/h
Operational range 3,530 km 3,000 km
Service ceiling 18,500 m 17,500 m
Max. takeoff weight 30,000 kg 33,000 kg
Empty weight 16,300 kg 17,700 kg
Total thrust 2 x 12,502 kgf 2 x 12,500 kgf
Performance Radar Chart

Detailed Comparison

The Su-27 Flanker was developed as a dedicated air superiority fighter to counter its Western counterparts, while the Su-30 Flanker-C is a direct evolution, transforming the single-seat airframe into a two-seat, multirole combat aircraft. This fundamental difference in mission dictates their design, capabilities, and operational use. The Su-27 established the Flanker's reputation for exceptional agility and long range, whereas the Su-30 builds upon that foundation, adding significant air-to-ground strike and command capabilities.

Development and Design

The Su-27's design philosophy prioritized kinematic performance. Its blended wing-body and large internal fuel capacity provided a combination of high maneuverability and extended range, making it a formidable air-to-air platform. Development focused on achieving superiority over the F-15 Eagle.

The Su-30's genesis lies in the Su-27UB two-seat trainer. The potential for a second crew member to manage complex missions, particularly long-range interception and ground-attack, was recognized. This led to the Su-30. Key export variants like the Su-30MKI introduced critical innovations not present on the original Su-27, including:

  • Canards: Forward-mounted control surfaces that significantly improve maneuverability and control at high angles of attack.
  • Thrust-Vectoring Nozzles: These allow the pilot to direct engine thrust, granting extreme agility in dogfights.
  • Second Crew Member: A Weapon Systems Officer (WSO) in the rear seat manages navigation, targeting pods, and complex guided munitions, reducing the pilot's workload.

Specifications and Performances

While sharing the same basic airframe, their performance metrics reflect their differing roles. The original Su-27 is lighter (16,300 kg empty weight vs. 17,700 kg for the Su-30) and boasts a higher top speed (2500 km/h vs. 2125 km/h) and service ceiling. This is consistent with its specialization as a pure air interceptor. In contrast, the Su-30 has a significantly higher Maximum Takeoff Weight (33,000 kg vs. 30,000 kg), allowing it to carry more fuel and a heavier, more diverse weapons payload on its 12 hardpoints. The Su-30's AL-31FP engines, featured on advanced variants, provide thrust vectoring, a capability the baseline Su-27 lacks.

Deployment and usage

The Su-27's operational history, such as its use by Ethiopia in the Eritrean-Ethiopian War, highlights its effectiveness in its intended air superiority role, securing air dominance. Russian Su-27s have primarily served in air defense and patrol missions. The Su-30, however, is employed more broadly. The Indian Air Force uses its Su-30MKI fleet for a wide spectrum of missions, from air defense and long-range strike to maritime patrol and nuclear delivery. Similarly, China's Su-30MKK variant was specifically acquired to bolster its maritime strike capabilities. The two-seat configuration makes the Su-30 a more suitable platform for complex, long-endurance missions requiring intensive sensor and weapons management.

Conclusion

The Su-27 remains a highly capable air superiority fighter, defined by its speed, altitude, and agility. The Su-30 represents a logical and highly successful evolution, sacrificing some peak kinematic performance for immense multirole flexibility. Its primary advancements—the two-person crew, sophisticated avionics, and expanded payload for precision air-to-surface munitions—make it a far more versatile asset on the modern battlefield. The addition of the WSO is the most critical differentiator, enabling the platform to effectively employ its advanced systems in complex combat environments where a single pilot would be task-saturated.

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Frequently Asked Questions

Which is faster, the Su-27 Flanker or Su-30 Flanker-C?
The Su-27 Flanker is faster with a maximum speed of 2,500 km/h compared to the Su-30 Flanker-C's 2,125 km/h, a difference of 375 km/h.
Which has longer range, the Su-27 Flanker or Su-30 Flanker-C?
The Su-27 Flanker has a longer range at 3,530 km compared to the Su-30 Flanker-C's 3,000 km.
Which can fly higher, the Su-27 Flanker or Su-30 Flanker-C?
The Su-27 Flanker has a higher service ceiling at 18,500 meters (60,695 ft) compared to the Su-30 Flanker-C's 17,500 meters (57,414 ft).
Which is heavier, the Su-27 Flanker or Su-30 Flanker-C?
The Su-30 Flanker-C has a higher maximum takeoff weight at 33,000 kg compared to the Su-27 Flanker's 30,000 kg.
Which is larger, the Su-27 Flanker or Su-30 Flanker-C?
The Su-30 Flanker-C is longer at 21.9 meters compared to the Su-27 Flanker's 21.9 meters.
Which is more expensive, the Su-27 Flanker or Su-30 Flanker-C?
The Su-30 Flanker-C is more expensive at approximately $37 million per unit compared to the Su-27 Flanker at $30 million.
Which entered service first, the Su-27 Flanker or Su-30 Flanker-C?
The Su-27 Flanker entered service first in 1985, 11 years before the Su-30 Flanker-C which entered service in 1996.
Which has been built in greater numbers, the Su-27 Flanker or Su-30 Flanker-C?
The Su-27 Flanker has been produced in greater numbers with 680 units compared to 630 units of the Su-30 Flanker-C.