The A-4M Skyhawk, flown by Marine Attack Squadron 311 (VMA-311), represented the ultimate refinement of the Douglas A-4 series, purpose-built for U.S. Marine Corps ground-attack operations. Introduced in the early 1970s, the A-4M featured substantial improvements in engine power, avionics, survivability, and pilot ergonomics, making it the most advanced Skyhawk variant ever produced.
Driven by a Pratt & Whitney J52-P-408 turbojet engine, the A-4M boasted improved thrust, offering a top speed of approximately 673 mph (1,083 km/h). Its robust design allowed for a maximum ordnance load of 9,900 lbs (4,490 kg) across five external hardpoints, enabling it to carry a wide array of bombs, rockets, and missiles—including the AGM-45A Shrike anti-radiation missile.
VMA-311, nicknamed the "Tomcats", effectively deployed the A-4M in both training and operational contexts, particularly in close air support and strike missions. The squadron’s proficiency combined with the Skyhawk’s nimble performance helped define U.S. Marine air-ground tactics in the late Cold War period.
Key features and upgrades of the A-4M included:
Dorsal avionics "hump" housing advanced electronics and navigation systems.
Upgraded cockpit with a heads-up display (HUD), enlarged canopy, and improved ejection seat.
Enhanced survivability, including increased armor and countermeasure systems.
More powerful engine for improved climb rate and payload performance.
Controls:
AG1: Jettison fuel tank
AG2: Jettison AGM-45A
AG7: Extend tail hook
AG8: Light
VTOL: Flaps
Trim: Elevator Trim
Credits: @Inuyasha8215
Specifications
General Characteristics
- Predecessor A-4F Skyhawk VA-164
- Created On Android
- Wingspan 17.2ft (5.2m)
- Length 26.8ft (8.2m)
- Height 11.9ft (3.6m)
- Empty Weight N/A
- Loaded Weight 6,863lbs (3,113kg)
Performance
- Power/Weight Ratio 1.355
- Wing Loading 21.2lbs/ft2 (103.5kg/m2)
- Wing Area 323.6ft2 (30.1m2)
- Drag Points 1289
Parts
- Number of Parts 354
- Control Surfaces 13
- Performance Cost 1,423