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Aviation / Aerospace

Douglas A-4 Skyhawk


Light Attack Multirole Carrierborne Fighter Aircraft [ 1956 ]



The Douglas A-4 Skyhawk naval jet fighter saw decades of service worldwide with nearly 3,000 aircraft produced.



Authored By: Staff Writer | Last Edited: 07/30/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

VIEW SPECIFICATIONS [+]
The A-4 Skyhawk (nicknamed "Heinemann's Hot Rod" and the "Scooter") came about as a private venture when the Douglas corporation was seeking to replace the aging AD Skyraider (A-1 Skyraider) piston-engine aircraft. The successor to the A-1 was originally another piston-engine alternative known by the designation as the A-2D Skyshark, but powerplant issues shelved the project altogether. During this time, the A-4 Skyhawk was already in development as a small, lightweight jet-powered attack aircraft to which the US Navy took a fair amount of interest in.

Ed Heinemann was the chief designer of the A-4 Skyhawk while working at Douglas, which led to the development of nine Skyhawk prototypes designated as the XA4D-1 - the first of which flew on September in 1956. From there, the Pratt & Whitney J65-powered craft would go into full operational production as the A-4A Skyhawk.

The Pratt & Whitney powerplant was a British-designed and licensed Armstrong Siddeley Sapphire turbojet. The system was capable of producing over 8,000lbs or standard thrust (no afterburner was integrated to the engine) and the base powerplant could be found on the initial three A-4's - the A, B and C models.

The A-4E Skyhawk model stood as a vast improvement over previous models and served the US Navy featuring an overall heavier airframe but a Pratt & Whitney J52 powerplant. A successive model for the US Navy, the A-4F, proved to be the last model and featured further improvements on the A-4E, most notably the avionics-housing "hump" visible in the image above just behind the cockpit and running along the dorsal spine of the fuselage.

The United States Marine Corps took orders for the "Ultimate Skyhawk" in the A-4M Skyhawk II. This model featured an all-new enlarged canopy for improved pilot visibility. It also featured an increased MTOW capacity (nearly double of what the base A-4 could do) allowing for an additional array of weaponry to be fitted. The A-4M model was fitted with an even more powerful J52-P-408 powerplant that increase range and overall speed.

Export figures were decent, with Argentina becoming the initial customer. Others would soon follow including Israel, Malaysia, Kuwait, Brazil and Singapore. In the end, the A-4 Skyhawk proved its worth with decades of faithful service to the United States with the Navy and the Marine Corps both putting the aircraft through a rigorous pacing. The single powerplant was more than suitable for the role that the A-4 was designed to fulfill and the diminutive size when compared to other carrier aircraft was a good fit for carrier storage.©MilitaryFactory.com
Note: The above text is EXCLUSIVE to the site www.MilitaryFactory.com. It is the product of many hours of research and work made possible with the help of contributors, veterans, insiders, and topic specialists. If you happen upon this text anywhere else on the internet or in print, please let us know at MilitaryFactory AT gmail DOT com so that we may take appropriate action against the offender / offending site and continue to protect this original work.

Specifications



McDonnell Douglas - USA
Manufacturer(s)
Argentina; Australia; Brazil; Indonesia; Israel; Malaysia; New Zealand; Singapore; United States
Operators National flag of Argentina National flag of Australia National flag of Brazil National flag of Indonesia National flag of Israel National flag of Malaysia National flag of New Zealand National flag of Singapore National flag of the United States
1956
Service Year
United States
National Origin
Retired
Project Status
1
Crew
2,960
Units


AIR-TO-AIR COMBAT
General ability to actively engage other aircraft of similar form and function, typically through guns, missiles, and/or aerial rockets.
GROUND ATTACK
Ability to conduct aerial bombing of ground targets by way of (but not limited to) guns, bombs, missiles, rockets, and the like.
MARITIME / NAVY
Land-based or shipborne capability for operating over-water in various maritime-related roles while supported by allied naval surface elements.
TRAINING
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).


40.3 ft
(12.27 meters)
Length
27.5 ft
(8.38 meters)
Width/Span
15.0 ft
(4.57 meters)
Height
10,465 lb
(4,747 kilograms)
Empty Weight
24,504 lb
(11,115 kilograms)
Maximum Take-Off Weight
+14,039 lb
(+6,368 kg)
Weight Difference


1 x Pratt & Whitney J52-P-408 non-afterburning turbojet developing 11,200 lb of thrust.
Propulsion
645 mph
(1,038 kph | 560 knots)
Max Speed
38,698 ft
(11,795 m | 7 miles)
Ceiling
2,001 miles
(3,220 km | 1,739 nm)
Range
10,300 ft/min
(3,139 m/min)
Rate-of-Climb


MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030


STANDARD, FIXED:
2 x 20mm Colt Mk 12 automatic internal cannons in wing roots (one gun per root).

OPTIONAL:
Mission-specific weapons included any of the following:

AIM-9 "Sidewinder" short-range air-to-air missiles.
AGM-12 "Bullpup" air-to-surface missiles.
AGM-65 "Maverick" air-to-surface missiles.
AGM-45 "Shrike" anti-radiation missiles.
AGM-62 "Walleye" glide drop bombs.
LAU-10 rocket pods.
B43, B57 and B61 nuclear bombs.
Rockeye Mk 7 (cluster), Rockeye II Mark 20 (cluster) and Mark 80 conventional drop bombs.
3 x 370 Gallon jettisonable fuel tanks.

Maximum ordnance loads of up to 9,155lb (4,155 kg) across five external hardpoints (1 x Fuselage centerline; 4 x Underwing); Three internal positions plumbed for fuel stores.


5 (including fuselage centerline)
Hardpoints


XA4D-1 - Prototype Designation of which nine produced.
A4D-1 - Initial Production Models pre-1962 reorganization.
A-4A - Initial production model post-1962 designation; 166 examples completed.
A-4B - Reinforced airframe; air-to-air capability added; improved avionics; AGM-12 Bullpup missile support; 542 examples completed.
A-4C - Adverse weather variant with AN/APG-53A radar; powered by Wright J65-W-20 engine of 8,200lb thrust; 638 examples produced.
A-4E - Refined variant; heavier airframe; powered by Pratt & Whitney J52 engine.
A-4F - Final USN variant with fuselage "hump" housing additional avionics equipment.
A-4M "Skyhawk II" - USMC variant with enlarged canopy for increased visibility; increased MTOW; more powerful J52-P-408 engine.
TA-4F - Two-seat USN trainer Variant
A-4P - Argentine Air Force export model
A-4Q - Argentine Air Force export model
A-4AR "Fightinghawks" - Argentine Air Force export model based on A-4M; updated avionics, HUD system and ARG-1 radar system.
A-4H - Israeli export model based on A-4E variant.
A-4N - Israeli export model based on A-4M variant.
A-4S - Singapore export model
A-4K - New Zealand export model with upgraded HUD, avionics, twin-CRT displays and HOTAS.
T/A-4KU - Kuwaiti export model (resold to Brazil).


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