Air Weapons

Attack (1956)

Douglas

A-4 Skyhawk

A-4B Skyhawk (USN, VA-55 'Warhorses')
A-4E

As the last major design by the great Ed Heinemann, the Douglas A-4 Skyhawk was one of the best examples of cramming the most capabilities into the smallest possible airframe for the intention of replacing the venerable A-1 in service with the US Navy's carrier fleets. It was given a number of nicknames throughout its career such as 'Heinemann's Hot Rod' and 'Scooter'; its design was characterized by small delta wings (thus eliminating the need for folding wings), side-mounted intakes, and a cruciform tail. Another notable feature was the inclusion of a buddy system of inflight refuelling thus eliminating the need for specialized tankers. Skyhawks were prominent during the early stages of the Vietnam War as the primary USN light attack aircraft until replaced by the larger A-7. Foreign Skyhawks also saw considerable action: Israeli units were used during the Yom Kippur War while Argentinian aircraft saw action in the Falklands sinking or damaging numerous British ships. More recently, Kuwaiti units were flown against Iraq during the 1991 Gulf War. Other foreign operators of the A-4 include Argentina, Brazil, Indonesia, Malaysia, New Zealand, and Singapore. Although USN A-4s were retired from front-line service in 1975, they continued to fly in various support roles, most notably as a special aggressor trainer aircraft.

The first flight of the prototype XA4D-1 took place on 22 June 1954 followed by the production A4D-1 (known after 1962 as the A-4A) which were the first to equip USN squadrons. Later, the A4D-2 (A-4B) had a new version of the J65 engine, aerial refuelling, and a number of structural improvements and was also given all-weather capability in the radar-equipped A4D-2N (A-4C). These would later be upgraded to A-4L standards with new engines and a dorsal hump housing new avionics. The next series of Skyhawks began with the A4D-5 (A-4E) with J52 engines, new structures, and additional hardpoints. The last USN version was the A-4F with a similar dorsal hump as the A-4L among other improvements while the A-4M Skyhawk II was built for the USMC with new modern avionics and what was said to be a 30 percent improvement in combat efficiency to its predecessors. Exported versions were generally based on their US counterparts, these were the A-4P and -4Q for Argentina (based on the B and C) and the A-4G (Australia), A-4H (Israel), A-4K (New Zealand) all of which were based on the A-4F. The A-4M resulted in the A-4N (Israel), A-4KU (Kuwait), A-4AR (Argentina), and the AF-1 (Brazil). Numerous other trainer versions were built including the TA-4E, -4F, and -4F as well as similarly designated versions of foreign aircraft. while a forward air control variant was known as the OA-4M.

Preceded by:

A-1 Skyraider (1946)

Succeeded by:

A-7 Corsair II (1967)

Datafile

DesignA-4BA-4EA-4FA-4M
NameSkyhawkSkyhawkSkyhawkSkyhawk II
TypeAttackAttackAttackAttack
Year1957196219671971
Crew1111
Dimensions
Length39 ft 4 in40 ft 4 in40 ft 3 in40 ft 4 in
Height14 ft 12 in14 ft 12 in14 ft 12 in14 ft 12 in
Wing Span26 ft 6 in26 ft 6 in26 ft 6 in26 ft 6 in
Wing Arean/an/an/an/a
Weight
Empty9,146 lbs9,624 lbs10,450 lbs10,800 lbs
Maximum22,500 lbs22,950 lbs24,500 lbs27,420 lbs
Wing Loading86.5 lb/ft²88.3 lb/ft²94.2 lb/ft²105.5 lb/ft²
Performance
Speed649 mph673 mph675 mph670 mph
Ceiling41,800 ft40,050 ft42,250 ft42,260 ft
Range1,000-1,650 mi2,130 mi2,000 mi2,050 mi
Powerplant
Engine1 x J65-W-16
Wright
7,700 lbf
1 x J52-P-6A
Pratt & Whitney
8,500 lbf
1 x J52-P-8A
Pratt & Whitney
9,300 lbf
1 x J52-P-408
Pratt & Whitney
11,200 lbf
Thrust/Weight0.770.800.810.94
Armament
Guns2 x 20-mm
Colt Mk. 12 (100)
2 x 20-mm
Colt Mk. 12 (100)
2 x 20-mm
Colt Mk. 12 (100)
2 x 20-mm
Colt Mk. 12 (100)
Payload5,975 lbs8,200 lbs8,200 lbs9,155 lbs
Hardpoints3555
AA Weapons-AIM-9
AIM-9
AIM-9
AS WeaponsAGM-12
AGM-62
Mk. 82/83/84
AGM-12
AGM-45
AGM-62
Mk. 82/83/84
AGM-12
AGM-45
AGM-62
Mk. 82/83/84
AGM-12
AGM-45
AGM-62
AGM-65
Mk. 82/83/84
Production
Built542499147158
Total2,690

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