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A-6 Intruder vs A-7 Corsair II

A-6 Intruder vs A-7 Corsair II at a glance — top speed 1,040 vs 1,123 km/h, range 5,219 vs 2,485 km, max takeoff weight 27,500 vs 19,050 kg, built 693 vs 1,545 units.

Grumman A-6 Intruder combat aircraft side profile drawing
🇺🇸 A-6 Intruder
Vought A-7 Corsair II combat aircraft side profile drawing
Specifications
A-6 Intruder A-7 Corsair II
Origin country 🇺🇸 United States 🇺🇸 United States
Category Combat Aircraft Combat Aircraft
Manufacturer Grumman Vought
First flight 19 April 1960 27 September 1965
Year introduced 1963 1966
Number produced 693 units 1545 units
Average unit price $25 million $2 million
Wing area 49.1 m² 34.8 m²
Wingspan 16.2 m 11.8 m
Height 4.8 m 4.9 m
Length 16.6 m 14.1 m
Maximum speed 1040 km/h 1123 km/h
Operational range 5,219 km 2,485 km
Service ceiling 12,400 m 12,800 m
Max. takeoff weight 27,500 kg 19,050 kg
Empty weight 11,630 kg 8,840 kg
Total thrust 2 x 8,436 kgf 1 x 6,795 kgf
Performance Radar Chart

Detailed Comparison

The Grumman A-6 Intruder and LTV A-7 Corsair II divided the U.S. Navy’s strike mission into two tiers based on procurement cost, aircrew configuration, and avionics architecture. The A-6 was a $25 million twin-engine, two-seat platform engineered for deep, radar-guided night interdiction. The A-7 emerged from the VAL requirement as a $2 million single-seat derivative of the F-8 Crusader, built to replace the A-4 Skyhawk in volume.

Development and Design

Grumman optimized the A-6 around the DIANE suite, pairing a pilot and bombardier/navigator side-by-side to process analog computing data and terrain-mapping radar for blind-bombing. This mandated a wide, drag-inducing fuselage. LTV bypassed radar complexity in the A-7 to minimize R&D risk, shortening the F-8 airframe and replacing the variable-incidence wing with a fixed structure. Where the A-6 relied on a second crew member, the A-7 shifted the pilot's workload to early head-up displays and a continuous-solution navigation and weapons delivery computer. The A-7 also transitioned from turbojets to turbofans, adopting the TF30 and later TF41 for unrefueled endurance, while the A-6 retained less fuel-efficient J52 turbojets.

Specifications and Performances

The structural and aerodynamic differences between the two airframes dictated their operating parameters:

  • The A-6 carried an 18,000 lb payload, enabled by a 27,500 kg maximum takeoff weight.
  • The A-7 lifted a 15,000 lb payload, constrained by a 19,050 kg MTOW.
  • The A-7 extracted a 279 km range advantage (1,981 km versus 1,702 km) over the A-6, utilizing a single turbofan engine and a low-drag frontal profile.

The A-7’s TF41 engine struggled with thrust generation in high-temperature, high-humidity environments, extending takeoff rolls when fully laden. The A-6 compensated for the poor fuel fraction of its J52 turbojets through volume, accommodating large internal tanks and up to five 300-gallon external drops.

Deployment and usage

Both airframes sustained heavy exposure during the Vietnam War. The A-6 executed night and monsoon-weather strikes along the Ho Chi Minh Trail. This profile forced low-altitude ingress and resulted in 84 combat losses to conventional ground fire. The A-7, arriving in theater later, executed daylight interdiction. The A-7’s digital weapons delivery computer generated hit rates that prompted the U.S. Air Force to procure the A-7D, bypassing their traditional preference for supersonic fighters. In operations over Lebanon, Libya, and Iraq, the A-6 functioned as the primary deep-strike asset and organic aerial tanker, while the A-7 specialized in defense suppression, launching AGM-88 HARMs.

Conclusion

The A-6 Intruder holds the absolute edge in deep, all-weather strike and maritime interdiction. Its twin-engine redundancy, payload capacity, and dedicated bombardier/navigator enabled blind-bombing profiles that single-seat aircraft of the era could not execute. Conversely, the A-7 Corsair II was the better platform for force structure economics and daytime tactical strike. By carrying 80% of the Intruder's payload at less than 10% of the unit cost, the A-7 allowed the Pentagon to generate sortie volume and shift the single-seat attack doctrine toward digital computer-aided precision.

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Frequently Asked Questions

Which is faster, the A-6 Intruder or A-7 Corsair II?
The A-7 Corsair II is faster with a maximum speed of 1,123 km/h compared to the A-6 Intruder's 1,040 km/h, a difference of 83 km/h.
Which has longer range, the A-6 Intruder or A-7 Corsair II?
The A-6 Intruder has a longer range at 5,219 km compared to the A-7 Corsair II's 2,485 km.
Which can fly higher, the A-6 Intruder or A-7 Corsair II?
The A-7 Corsair II has a higher service ceiling at 12,800 meters (41,994 ft) compared to the A-6 Intruder's 12,400 meters (40,682 ft).
Which is heavier, the A-6 Intruder or A-7 Corsair II?
The A-6 Intruder has a higher maximum takeoff weight at 27,500 kg compared to the A-7 Corsair II's 19,050 kg.
Which is larger, the A-6 Intruder or A-7 Corsair II?
The A-6 Intruder is longer at 16.6 meters compared to the A-7 Corsair II's 14.1 meters.
Which is more expensive, the A-6 Intruder or A-7 Corsair II?
The A-6 Intruder is more expensive at approximately $25 million per unit compared to the A-7 Corsair II at $2.0 million.
Which entered service first, the A-6 Intruder or A-7 Corsair II?
The A-6 Intruder entered service first in 1963, 3 years before the A-7 Corsair II which entered service in 1966.
Which has been built in greater numbers, the A-6 Intruder or A-7 Corsair II?
The A-7 Corsair II has been produced in greater numbers with 1,545 units compared to 693 units of the A-6 Intruder.