McDonnell Douglas A-4 Skyhawk
Summary
Category | Combat aircraft |
Origin country | 🇺🇸 United States |
First flight | 22 June 1954 |
Year of introduction | 1956 |
Number produced | 2960 units |
Average unit price | $2 million |
Description
The A-4 Skyhawk is a single-seat subsonic carrier-capable attack aircraft developed for the United States Navy and United States Marine Corps in the early 1950s. The delta winged, single turbojet-engined Skyhawk was designed and produced by Douglas Aircraft Company, and later by McDonnell Douglas. It was originally designated A4D under the U.S. Navy's pre-1962 designation system.
The development and design of the A-4 Skyhawk were marked by the emphasis on simplicity and efficiency. The aircraft was designed to meet a Navy requirement for a carrier-based, single-seat attack aircraft. It was a compact, light-weight design powered by a single Wright J65 turbojet engine. The Skyhawk's small size allowed it to be stored on an aircraft carrier without folding its wings, and it was capable of carrying a substantial payload. The design proved to be versatile and adaptable, and the Skyhawk served the Navy and Marine Corps in a variety of roles throughout its service life.
Armament
- Cannons: Two 20mm cannons, integrated into the wing roots, provided basic self-defense capabilities against enemy aircraft.
- Missiles: Later variants of the A-4 were equipped with AIM-9 Sidewinder missiles, enhancing their air-to-air combat potential.
- Bombs: The A-4 could carry a payload of bombs, ranging from small 250-pounders to 1,000-pounders. It even had the capability to deliver nuclear weapons using specialized delivery techniques.
- Rockets: For close-in attacks and area suppression, the Skyhawk could be equipped with multiple pods firing 70mm or 127mm rockets, raining down firepower on enemy positions.
- Napalm: During the Vietnam War, the A-4 became notorious for its use of napalm, delivering devastating aerial incendiary attacks.
Operational history
The A-4 Skyhawk has a rich operational history, serving in numerous conflicts worldwide. It first saw combat in the Vietnam War, where it was used by both the U.S. Navy and Marine Corps for ground-attack missions. The Skyhawk played a crucial role in many key operations throughout the war, and its performance garnered praise for its reliability and effectiveness.
Following its service in Vietnam, the A-4 Skyhawk continued to serve in various capacities in the U.S. armed forces. It was used in training roles, preparing generations of pilots for combat. The aircraft also saw service with the Blue Angels, the U.S. Navy's flight demonstration squadron, further demonstrating its versatility and durability.
Internationally, the A-4 Skyhawk was widely exported and saw service with various foreign militaries. It was used extensively by the Israeli Air Force, playing a pivotal role in several Middle Eastern conflicts. The Skyhawk was also operated by several other nations, including Argentina, Brazil, and New Zealand.
Variants
- A-4A: This was the initial production version, featuring the Wright J65-W-4 turbojet engine, and equipped with 2× 20 mm Colt Mk 12 cannons.
- A-4B: Introduced in 1957, this variant included notable improvements such as air-to-air refueling capabilities and an improved navigation system.
- A-4C: The A-4C was the first version to include an all-weather capability, and it introduced a more powerful Wright J65-W-20 engine.
- A-4E: This model had an upgraded engine, two additional weapons pylons, and improved avionics.
- A-4F: The A-4F was an improved version of the A-4E, featuring an even more powerful engine and extra avionics housed in a distinctive hump on the fuselage.
- A-4G: This was a specialized version for the Royal Australian Navy, with anti-submarine capabilities.
- A-4H: The A-4H was a version produced for the Israeli Air Force, featuring improved avionics and the ability to carry a larger payload.
- A-4M: The A-4M was an improved version specifically for the Marine Corps, with further upgraded avionics and a more powerful engine.
Technical specifications
Version: A-4F | |
---|---|
Crew | 1 pilot |
Operational range | 3300 km (2051 mi) |
Maximum speed | 1077 km/h (669 mph) |
Wing area | 24.2 m² (259.9 sqft) |
Wingspan | 8.4 m (27.5 ft) |
Height | 4.6 m (15.0 ft) |
Length | 12.2 m (40.1 ft) |
Service ceiling | 12880 m (42257 ft) |
Empty weight | 4750 kg (10472 lbs) |
Max. takeoff weight | 11136 kg (24551 lbs) |
Climb rate | 43.0 m/s (141.1 ft/s) |
Powerplant | 1 × turbojet Pratt & Whitney J52-P8A delivering 4100 kgp |
Ejection seat | Escapac IC-3 |
Current operating countries
Country | Units | ||
---|---|---|---|
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Argentina | 27 | |
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Brazil | 6 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.
All operators
Argentina • Australia • Brazil • Indonesia • Israel • Kuwait • Malaysia • New Zealand • Singapore • United States
Armament
Missiles payload:
- Air-to-Surface AGM-12 Bullpup
- Anti-Radiation AGM-45 Shrike
- Air-to-Surface AGM-65 Maverick
- Air-to-Air Short-Range Raytheon AIM-9 Sidewinder
Bombs payload:
- Thermonuclear B57 Mod 1
- Thermonuclear B61
- Cluster CBU-59/B Rockeye II
- Cluster Mk 20 Mod 0 Rockeye
Photo of A-4 Skyhawk

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