Name | A-4S-1 "Super Skyhawk"(McDonnell Douglas Aircraft ) |
Type | Attack and CAS (Close Air Support) |
Year | October 1956 |
Engine | One General Electric F404-GE-100D non-afterburning turbofan |
Length | 12.72 m |
Height | 4.57 m |
Ceiling | 12,190m |
Weight | 10,206 kg |
Speed | 1,128 km /h |
Max. Range | 625 nm (1,158 km) |
Wing span | 8.38 m |
Crew | 1 |
Armament | Two Mk 12 20-mm cannon in
wingroots;
plus ordnance including : bombs,
|
Early models comprised the Wright J65-W2 powered A-4A/B/Cs (differing
in avionics and engine power), the Pratt & Whitney J52-P
engined A-4Es and A-4Fs with a dorsal avionics hump. Export models
comprised A-4G (Australia), A-4H (Israel), A-4K (New
Zealand), A-4KU (Kuwait) and A-4P & 4Q (Argentina). The A-4L was
a re-built A-4C for the USN Reserve. A-4Ns were similar to the
A-4H but featured uprated avionics, including a HUD. The last major
production model was the A-4M, based on the A-4F but
introducing a Pratt & Whitney J52-P-408 engine.
A-4 trainer variants feature two cockpits in tandem with a single canopy,
and some combat capability. The USMC's OA-4M was
used for FAC duties, and has been retired. The definitive TA-4J was
a simplified version which lacks cannon armament and combat
capability. In USN service this is the major operational model, used
for advanced training, including carrier qualification.
Singapore has the most capable Skyhawks, having upgraded surplus A-4B/Cs
as A-4Ss. Three modification standards exist: the
basic refurbished aircraft, the A-4S-1 Super Skyhawk, re-engined with
the GE-F404 turbofan, and the A-4SU with F404 and a new
digital avionics suite which include a Pave Penny laser designator,
pilot's HUD and an inertial navigation system (INS).
Source-McDonnell Douglas