A-4AL Fightinghawk
From Themarshallwiki
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*Wingspan: 27 ft 6 in (8.38 m) | *Wingspan: 27 ft 6 in (8.38 m) | ||
*Height: 14 ft 11 in (4.57 m) | *Height: 14 ft 11 in (4.57 m) | ||
| - | *Wing area: 259 | + | *Wing area: 259 ft<sup>2</sup> (24.15 m<sup>2</sup>) |
*Empty weight: 4,900 kg (10,803 lbs) | *Empty weight: 4,900 kg (10,803 lbs) | ||
*Loaded weight: 11,000 kg (24,251 lbs) | *Loaded weight: 11,000 kg (24,251 lbs) | ||
*Max takeoff weight: 24,500 lb (11,136 kg) | *Max takeoff weight: 24,500 lb (11,136 kg) | ||
| - | *Powerplant: | + | *Powerplant: 1 x General Electric F404-GE-100D turbofan, 10,800 lbf (48.4 kN) |
==Performance== | ==Performance== | ||
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*Service ceiling: 42,250 ft (12,880 m) | *Service ceiling: 42,250 ft (12,880 m) | ||
*Rate of climb: 8,440 ft/min (43 m/s) | *Rate of climb: 8,440 ft/min (43 m/s) | ||
| - | *Wing loading: 70.7 lb/ | + | *Wing loading: 70.7 lb/ft<sup>2</sup> (344.4 kg/m<sup>2</sup>) |
*Thrust/weight: 0.55 | *Thrust/weight: 0.55 | ||
==Armament== | ==Armament== | ||
| - | *Guns: | + | *Guns: 2 x 20 mm (0.787 in) Colt Mk 12 cannon, 100 rounds/gun |
*Air to Air Missiles: Rafael Python, Rafael Derby, AGM-65 Maverick, AM.39 Exocet, Popeye Lite, SNEB rockets, | *Air to Air Missiles: Rafael Python, Rafael Derby, AGM-65 Maverick, AM.39 Exocet, Popeye Lite, SNEB rockets, | ||
*Bombs: 9,900 lb (4,490 kg) on five external hardpoints | *Bombs: 9,900 lb (4,490 kg) on five external hardpoints | ||
Revision as of 02:02, 10 July 2009
The A-4AL Fightinghawk is used by both the Navy, and Air Force. The Fightinghawk is an upgraded A-4M Skyhawk originally manufactured by McDonnell Douglas. The Fightinghawk upgrade was a joint project of Lockheed Martin and FMA. In the Air Force, the Fightinghawk serves as a ground attack aircraft, while the Navy use it as a fighter, with the secondary roles of ground attack and maritime strike.
The ECAL Armed Forces acquired their first Skyhawks in 1965, with the Air Force operating the A-4P in the ground attack role, and the Navy operating the A-4Q as sole combat aircraft. Arms embargoes enforced by the United States as well as a bad economic situation prevented resupply of the Skyhawks with the result (in the Air Force) of a much reduced capability. The Navy turned to the Super Etendard, although the Mitterand government stopped full deliveries.
After the return of democracy, and the repair of the civil-military relationship, the way to rearmament was opened. While some countries were hesitant to sell such items as armoured vehicles (which could be used against demonstrators), jet aircraft were not useful for internal suppression. The Air Force examined the Brazilian-Italian AMX, but it was found to be too expensive. In addition, there was no Latin American industry participation, and the absence of a Naval version meant that it was only a half solution.
In 1994, the United States made an offer. It would supply two hundred and eighty refurbished A-4M and TA-4M Skyhawks to the Government of the Confederate States of Latin America in a two billion dollar deal that would involve an almost total upgrade of the A-4M/TA-4M Skyhawks to be carried out by Lockheed Martin and FMA. It was the most ambitious project undertaken by FMA, and gave good experience for the F-90 Halcon program.
The Fightinghawk is one of the most sophisticated military aircraft in Latin America. In terms of American naval aircraft, its only real rivals are from the United States.
Contents |
Technical Information
The A-4AL Fightinghawks were sourced from the AMARC in Arizona. Upgrade plans included:
- Complete overhaul of the airframe, and the wiring looms
- Installation of a non-afterburning General Electric F404-GE-100D turbofan engine
- Installation of Douglas Escapac 1-G3 ejection seats
- HGU-55/P helmets
- Honeywell Normal Air-Garrett's OBOGS (On Board Oxygen Generation System)
- Westinghouse/Northrop Grumman AN/APG-66V2 (ARG-1) radar
- HOTAS controls and a 'glass' cockpit (2 CRT color screens)
- Sextant Avionique/Thales Avionics SHUD
- Litton/Northrop Grumman LN-100G inertial navigation system
- MIL-STD-1553B data bus
- Two General Dynamics Information Systems AN/AYK-14 mission computers
- Northrop Grumman AN/ALR-93 (V)1 Radar warning receiver
- AN/ALQ-126B jammer
- ALR-47 chaff/flare dispenser
- IFF AN/APX-72
Several extra airframes were acquired for spare parts, and test flying.
Specifications
General characteristics
- Crew: 1 (2 in TA-4AL)
- Length: 40 ft 3 in (12.30 m)
- Wingspan: 27 ft 6 in (8.38 m)
- Height: 14 ft 11 in (4.57 m)
- Wing area: 259 ft2 (24.15 m2)
- Empty weight: 4,900 kg (10,803 lbs)
- Loaded weight: 11,000 kg (24,251 lbs)
- Max takeoff weight: 24,500 lb (11,136 kg)
- Powerplant: 1 x General Electric F404-GE-100D turbofan, 10,800 lbf (48.4 kN)
Performance
- Maximum speed: 1128 km/h (609 kts, 701 mph)
- Range: 1,700 nm (2,000 mi, 3,220 km ferry range with 3 drop tanks)
- Service ceiling: 42,250 ft (12,880 m)
- Rate of climb: 8,440 ft/min (43 m/s)
- Wing loading: 70.7 lb/ft2 (344.4 kg/m2)
- Thrust/weight: 0.55
Armament
- Guns: 2 x 20 mm (0.787 in) Colt Mk 12 cannon, 100 rounds/gun
- Air to Air Missiles: Rafael Python, Rafael Derby, AGM-65 Maverick, AM.39 Exocet, Popeye Lite, SNEB rockets,
- Bombs: 9,900 lb (4,490 kg) on five external hardpoints
Images
Cockpit
Cockpit
General arrangement
