Width/Span
27.5 ft
(8.38 m)
Empty Wgt
10,465 lb
(4,747 kg)
MTOW
24,504 lb
(11,115 kg)
Wgt Diff
+14,039 lb
(+6,368 kg)
(Showcased structural values pertain to the Douglas A-4M Skyhawk II (Super Skyhawk) production variant)
Installed:
1 x Pratt & Whitney J52-P-408 non-afterburning turbojet developing 11,200 lb of thrust.
Max Speed
645 mph
(1,038 kph | 560 kts)
Ceiling
38,698 ft
(11,795 m | 7 mi)
Range
2,001 mi
(3,220 km | 5,963 nm)
Rate-of-Climb
10,300 ft/min
(3,139 m/min)
♦ 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
(Showcased performance specifications pertain to the Douglas A-4M Skyhawk II (Super Skyhawk) production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)
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.
(Not all ordnance types may be represented in the showcase above)
Hardpoint Mountings: 5 (including fuselage centerline)
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