McDONNELL DOUGLAS A-4 SKYHAWK
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The Douglas A-4 Skyhawk is a carrier-capable ground-attack aircraft designed for the United States Navy and United States Marine Corps. The delta winged, single turbojet-engined Skyhawk was designed and produced by Douglas Aircraft Company, and later McDonnell Douglas. It was originally designated the A4D under the US Navy's pre-1962 designation system.
Design and development
The Skyhawk was designed by Douglas Aircraft's Ed Heinemann in response to a U.S. Navy call for a jet-powered attack aircraft to replace the older AD Skyraider. Heinemann opted for a design that would minimize its size, weight, and complexity. The result was an aircraft that weighed only half of the Navy's weight specification. It had a wing so compact that it did not need to be folded for carrier stowage. The diminutive Skyhawk soon received the nicknames "Scooter", "Kiddiecar", "Bantam Bomber", "Tinker Toy Bomber", and, on account of its nimble performance, "Heinemann's Hot-Rod".
The aircraft is of conventional post-World War II design, with a low-mounted delta wing, tricycle undercarriage, and a single turbojet engine in the rear fuselage, with two air intakes on the fuselage sides. The tail is of cruciform design, with the horizontal stabilizer mounted above the fuselage. Armament consisted of two 20 mm (.79 in caliber) Colt Mk 12 cannons, one in each wing root, with 200 rpg, plus a large variety of bombs, rockets, and missiles carried on a hardpoint under the fuselage centerline and hardpoints under each wing (originally one per wing, later two).
The choice of a delta wing, for example, combined speed and maneuverability with a large fuel capacity and small overall size, thus not requiring folding wings, albeit at the expense of cruising efficiency. The leading edge slats were designed to drop automatically at the appropriate speed by gravity and air pressure, saving weight and space by omitting actuation motors and switches. Similarly the main undercarriage did not penetrate the main wing spar, designed so that when retracted only the wheel itself was inside the wing and the undercarriage struts were housed in a fairing below the wing. The wing structure itself could be lighter with the same overall strength and the absence of a wing folding mechanism further reduced weight. This is the opposite of what can often happen in aircraft design where a small weight increase in one area leads to a compounding increase in weight in other areas to compensate, leading to the need for more powerful, heavier engines and so on in a vicious circle
The A-4 pioneered the concept of "buddy" air-to-air refueling. This allows the aircraft to supply others of the same type, eliminating the need of dedicated tanker aircraft—a particular advantage for small air arms or when operating in remote locations. This allows for greatly improved operational flexibility and reassurance against the loss or malfunction of tanker aircraft, though this procedure reduces the effective combat force on board the carrier. A designated supply A-4 would mount a center-mounted "buddy store", a large external fuel tank with a hose reel in the aft section and an extensible drogue refueling bucket. This aircraft was fueled up without armament and launched first. Attack aircraft would be armed to the maximum and given as much fuel as was allowable by maximum takeoff weight limits, far less than a full tank. Once airborne, they would then proceed to top off their fuel tanks from the tanker using the A-4's fixed refueling probe on the starboard side of the aircraft nose. They could then sortie with both full armament and fuel loads. While rarely used in U.S. service since the KA-3 Skywarrior tanker became available, the F/A-18E/F Super Hornet includes this capability.
The A-4 was also designed to be able to make an emergency landing, in the event of a hydraulic failure, on the two drop tanks nearly always carried by these aircraft. Such landings resulted in only minor damage to the nose of the aircraft which could be repaired in less than an hour. Ed Heinemann is credited with having a large "K.I.S.S." sign put up on the wall of the drawing office when the aircraft was being designed. Whether or not this is true, the A-4 certainly is a shining example of the application of that principle to aircraft design.
The Navy issued a contract for the type on 12 June 1952, and the first prototype first flew from Edwards Air Force Base, California on 22 June 1954. Deliveries to Navy and Marine Corps squadrons (to VA-72 and VMA-224 respectively) commenced in late 1956.
The Skyhawk remained in production until 1979, with a total of 2,960 aircraft built, including 555 two-seat trainers.The last production A-4, an A-4M issued to a Marine squadron (VMA-223) had the flags of all nations who had operated the A-4 series aircraft painted on the fuselage sides.
The McDonnell Douglas A-4 "Skyhawk" in Viet Nam
The A-4 Skyhawk carried the battle to the enemy for the U.S. Navy and Marines. Skyhawk models A-4B, A-4C, A-4E, A-4F and TA-4F were involved in the conflict.
A-4 Skyhawk Pilots were in on the action from the very first air strikes in Vietnam, to the very last days of the conflict.
Total Navy Air Losses = 854 Aircraft, 575 Fatalities and 144 POWs.
Of these, 271 (31.7%) were Skyhawks, with 98 (17%) Skyhawk Fatalities and 48 (33%) Skyhawk POWs.
Total Marine Air Loses = 271 Aircraft, 241 Fatalities and 12 POWs.
Of these, 91 (33.6%) were Skyhawks, with 32 (13.3%) Skyhawk Fatalities and 1 (8.3%) Skyhawk POW.
Skyhawk losses to MiGs = 1, to SAMs = 32. Total A-4s lost in combat was 195.
As one would expect statistics vary based upon source. One claims 282 lost during the conflict, 195 of them in combat. But the above stats appear to be the most accurate.
First Skyhawk loss was A-4C 149578 from VA-144 aboard the USS Constellation, struck by AAA on 05AUG64, flown by LTJG Everett Alvarez who became the first, and longest held, POW of the conflict.
Final Skyhawk loss was A-4F 155021 from VA-212 aboard the USS Hancock, struck by AAA on 06SEPT72, the pilot, LT W.F. Pear was rescued.
A-4 displayed in Viet Nam :
01 AUG 1963 | 10 MAR 1964 | USS Oriskany CVA-34 | CVW-16 | VA-163 | A-4B |
| | | | VA-164 | A-4B |
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17 OCT 1963 | 20 JUL 1964 | USS Kitty Hawk CVA-63 | CVW11 | VA-112 | A-4C |
| | | | VA-113 | A-4C |
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28 JAN 1964 | 21 NOV 1964 | USS Bon Homme Richard CVA-31 | CVW-19 | VA-192 | A-4C |
| | | | VA-193 | A-4C |
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14 APR 1964 | 15 DEC 1964 | USS Ticonderoga CVA-14 | CVW-5 | VA-55 | A-4E |
| | | | VA-65 | A-4E |
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05 MAY 1964 | 01 FEB 1965 | USS Constellation CVA-64 | CVW-14 | VA-144 | A-4C |
| | | | VA-146 | A-4C |
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05 AUG 1964 | 06 MAY 1965 | USS Ranger CVA-61 | CVW-9 | VA-93 | A-4C |
| | | | VA-94 | A-4C |
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21 OCT 1964 | 29 MAY 1965 | USS Hancock CVA-19 | CVW-21 | VA-216 | A-4E |
| | | | VA-216 | A-4C |
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23 OCT 1964 | 16 MAY 1965 | USS Yorktown CVS-10 | CVSG-55 | VMA-223 Det T | A-4C |
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07 DEC 1964 | 01 NOV 1965 | USS Coral Sea CVA-43 | CVW-15 | VA-153 | A-4C |
| | | | VA-155 | A-4E |
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20 FEB 1964 | 11 AUG 1964 | USS Bennington CVS-20 | CVSG-59 | VA-93 Det Q | A-4B |
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19 JUN 1964 | 16 DEC 1964 | USS Kearsarge CVS-33 | CVSG-53 | VA-153 Det R | A-4B |
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06 MAR 1965 | 23 NOV 1965 | USS Midway CVA-41 | CVW-41 | VA-22 | A-4C |
| | | | VA-23 | A-4E |
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05 APR 1965 | 16 DEC 1965 | USS Oriskany CVA-34 | CVW-16 | VA-163 | A-4E |
| | | | VA-164 | A-4E |
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10 MAY 1965 | 13 DEC 1965 | USS Independence CVA-62 | CVW-7 | VA-72 | A-4E |
| | | | VA-86 | A-4E |
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21 APR 1965 | 13 JAN 1966 | USS Bon Homme Richard CVA-31 | CVW-9 | VA-192 | A-4C |
| | | | VA-195 | A-4C |
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12 AUG 1965 | 23 MAR 1966 | USS Hornet CVS-12 | CVSG-57 | H&MS-15 Det N | A-4C |
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28 SEP 1965 | 13 MAY 1966 | USS Ticonderoga CVA-14 | CVW-5 | VA-56 | A-4E |
| | | | VA-144 | A-4C |
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26 OCT 1965 | 21 JUN 1966 | USS Enterprise CVAN-65 | CVW-9 | VA-36 | A-4C |
| | | | VA-76 | A-4C |
| | | | VA-93 | A-4C |
| | | | VA-94 | A-4C |
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10 NOV 1965 | 01 AUG 1966 | USS Hancock CVA-19 | CVW-21 | VA-212 | A-4E |
| | | | VA-216 | A-4C |
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19 OCT 1965 | 13 JUN 1966 | USS Kitty Hawk CVA-63 | CVW-11 | VA-113 | A-4C |
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10 DEC 1965 | 25 AUG 1966 | USS Ranger CVA-61 | CVW-14 | VA-55 | A-4E |
| | | | VA-146 | A-4C |
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22 MAR 1965 | 07 OCT 1965 | USS Bennington CVS-20 | CVSG-59 | VA-113 Det Q | A-4B |
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04 APR 1966 | 21 NOV 1966 | USS Intrepid CVS-11 | CVW-10 | VA-15 | A-4B |
| | | | VA-95 | A-4B |
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12 MAY 1966 | 03 DEC 1966 | USS Constellation CVA-64 | CVW-15 | VA-153 | A-4C |
| | | | VA-155 | A-4E |
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26 MAY 1966 | 16 NOV 1966 | USS Oriskany CVA-34 | CVW-16 | VA-163 | A-4E |
| | | | VA-164 | A-4E |
21 JUN 1966 | 21 FEB 1967 | USS Franklin D. Roosevelt CVA-42 | CVW-42 | VA-12 | A-4E |
| | | | VA-72 | A-4E |
| | | | VA-172 | A-4C |
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29 JUL 1966 | 23 FEB 1967 | USS Coral Sea CVA-43 | CVW-2 | VA-22 | A-4C |
| | | | VA-23 | A-4E |
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15 OCT 1966 | 29 MAY 1967 | USS Ticonderoga CVA-14 | CVW-19 | VA-192 | A-4E |
| | | | VA-192 | A-4C |
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05 NOV 1966 | 19 JUN 1967 | USS Kitty Hawk CVA-63 | CVW-11 | VA-112 | A-4C |
| | | | VA-144 | A-4C |
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19 NOV 1966 | 06 JUL 1967 | USS Enterprise CVAN-65 | CVW-9 | VA-56 | A-4C |
| | | | VA-113 | A-4C |
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05 JAN 1967 | 22 JUL 1967 | USS Hancock CVA-19 | CVW-5 | VA-93 | A-4E |
| | | | VA-94 | A-4C |
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26 JAN 1967 | 25 AUG 1967 | USS Bon Homme Richard CVA-31 | CVW-21 | VA-76 | A-4C |
| | | | VA-212 | A-4E |
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29 APR 1967 | 04 DEC 1967 | USS Constellation CVA-64 | CVW-14 | VA-55 | A-4C |
| | | | VA-146 | A-4C |
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11 MAY 1967 | 30 DEC 1967 | USS Intrepid CVS-11 | CVW-10 | VSF-3 | A-4B |
| | | | VA-15 | A-4C |
| | | | VA-34 | A-4C |
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06 JUN 1967 | 15 SEP 1967 | USS Forrestal CVA-59 | CVW-17 | VA-46 | A-4E |
| | | | VA-106 | A-4E |
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16 JUN 1967 | 31 JAN 1968 | USS Oriskany CVA-34 | CVW-16 | VA-163 | A-4E |
| | | | VA-164 | A-4E |
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26 JUL 1967 | 06 APR 1968 | Uss Coral Sea CVA-43 | CVW-15 | VA-153 | A-4E |
| | | | VA-155 | A-4E |
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04 NOV 1967 | 25 MAY 1968 | USS Ranger CVA-61 | CVW-2 | VA-22 | A-4C |
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18 NOV 1967 | 28 JUN 1968 | USS Kitty Hawk CVA-63 | CVW-11 | VA-112 | A-4C |
| | | | VA-144 | A-4E |
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28 DEC 1967 | 17 AUG 1968 | USS Ticonderoga CVA-14 | CVW-19 | VA-23 | A-4F |
| | | | VA-192 | A-4F |
| | | | VA-192 | A-4C |
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03 JAN 1968 | 18 JUL 1968 | USS Enterprise CVAN-65 | CVW-9 | VA-56 | A-4E |
| | | | VA-113 | A-4F |
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27 JAN 1968 | 10 OCT 1968 | USS Bon Homme Richard CVA-31 | CVW-5 | VA-93 | A-4F |
| | | | VA-94 | A-4E |
| | | | VA-212 | A-4F |
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04 JUN 1968 | 08 FEB 1969 | USS Intrepid CVS-11 | CVW-10 | VA-36 | A-4C |
| | | | VA-66 | A-4C |
| | | | VA-106 | A-4E |
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18 JUL 1968 | 03 MAR 1969 | USS Hancock CVA-19 | CVW-21 | VA-55 | A-4F |
| | | | VA-163 | A-4E |
| | | | VA-164 | A-4E |
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07 SEP 1968 | 18 APR 1969 | USS Coral Sea CVA-43 | CVW-15 | VA-153 | A-4F |
| | | | VA-216 | A-4C |
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26 OCT 1968 | 17 MAY 1969 | USS Ranger CVA-61 | CVW-2 | VA-155 | A-4F |
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01 FEB 1969 | 18 SEP 1969 | USS Ticonderoga CVA-14 | CVW-16 | VA-112 | A-4C |
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18 MAR 1969 | 29 OCT 1969 | USS Bon Homme Richard CVA-31 | CVW-5 | VA-22 | A-4F |
| | | | VA-94 | A-4E |
| | | | VA-144 | A-4E |
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14 APR 1969 | 17 NOV 1969 | USS Oriskany CVA-34 | CVW-19 | VA-23 | A-4F |
| | | | VA-192 | A-4F |
| | | | VA-195 | A-4E |
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02 AUG 1969 | 15 APR 1970 | USS Hancock CVA-19 | CVW-21 | VA-55 | A-4F |
| | | | VA-164 | A-4F |
| | | | VA-212 | A-4F |
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05 MAR 1970 | 17 DEC 1970 | USS Shangri-la CVS-38 | CVW-8 | VA-12 | A-4C |
| | | | VA-152 | A-4E |
| | | | VA-172 | A-4C |
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02 APR 1970 | 12 NOV 1970 | USS Bon Homme Richard CVA-31 | CVW-5 | VA-22 | A-4F |
| | | | VA-94 | A-4E |
| | | | VA-144 | A-4F |
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22 OCT 1970 | 03 JUN 1971 | USS Hancock CVA-19 | CVW-21 | VA-55 | A-4F |
| | | | VA-164 | A-4F |
| | | | VA-212 | A-4F |
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07 JAN 1972 | 03 OCT 1972 | USS Hancock CVA-19 | CVW-21 | VA-55 | A-4F |
| | | | VA-164 | A-4F/TA-4F |
| | | | VA-212 | A-4F |
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08 MAY 1973 | 08 JAN 1974 | USS Hancock CVA-19 | CVW-21 | VA-55 | A-4F |
| | | | VA-164 | A-4F/TA-4F |
| | | | VA-212 | A-4F |
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18 MAR 1975 | 20 OCT 1975 | USS Hancock CVA-19 | CVW-21 | VA-55 | A-4F |
| | | | VA-164 | A-4F/TA-4F |
| | | | VA-212 |
General characteristics
- Crew: 1 (2 in OA-4F, TA-4F, TA-4J)
- Length: 40 ft 3 in (12.22 m)
- Wingspan: 26 ft 6 in (8.38 m)
- Height: 15 ft (4.57 m)
- Wing area: 259 ft² (24.15 m²)
- Airfoil: NACA 0008-1.1-25 root, NACA 0005-0.825-50 tip
- Empty weight: 10,450 lb (4,750 kg)
- Loaded weight: 18,300 lb (8,318 kg)
- Max takeoff weight: 24,500 lb (11,136 kg)
- Powerplant: 1× Pratt & Whitney J52-P8A turbojet, 9,300 lbf (10,000+ USMC A-4M and OA-4M) (41 kN)
Performance
- Maximum speed: 585 kn (673 mph, 1,077 km/h)
- Range: 1,700 nmi (2,000 mi, 3,220 km)
- Combat radius: 625 nmi, 1,158 km/h ()
- 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: 0.51
- g-limit: -3/+8 g
Armament
- Guns: 2× 20 mm (0.79 in) Colt Mk 12 cannon, 100 rounds/gun
- Hardpoints: 4× under-wing & 1× under-fuselage pylon stations holding up to 9,900 lb (4,490 kg) of payload
- Rockets:
- 4× LAU-10 rocket pods (each with 4× 127 mm Mk 32 Zuni rockets)
- Missiles:
- Air-to-air missiles:
- 4× AIM-9 Sidewinder
- Air-to-surface missiles:
- 2× AGM-12 Bullpup
- 2× AGM-45 Shrike anti-radiation missile
- 2× AGM-62 Walleye TV-guided glide bomb
- 2× AGM-65 Maverick
- Air-to-air missiles:
- Bombs:
- 6× Rockeye-II Mark 20 Cluster Bomb Unit (CBU)
- 6× Rockeye Mark 7/APAM-59 CBU
- Mark 80 series of unguided bombs (including 3 kg and 14 kg practice bombs)
- B57 nuclear bomb
- B61 nuclear bomb
- Others:
- up to 3× 300/330/370 US Gallon Sargent Fletcher drop tanks (pylon stations 2, 3, 4 are wet plumbed) for ferry flight/extended range/loitering time
Avionics
- Stewart-Warner AN/APQ-145 Mapping & Ranging radar (mounted on A-4F, also found on A-4E/N/S/SU)
- APN 141 Doppler Ground Radar (refitted to C and E, standard in the F)