It is 1947 and Ed Heinemann of the Douglas Aircraft Corporation is perplexed. Charged with leading the team that is designing Douglas’ entry in the Navy’s heavy attack aircraft competition, he is trying to figure out how to accomplish this feat in an airframe that would weigh in at less than 68,000 lbs, the maximum that the Midway-class carriers’ flight decks could sustain. His competitors over at Curtis and North American were gearing up for something closer to 100,000 lbs, a plane that would easily be accommodated on the Navy’s first supercarrier, the United States. Complicating his figuring was the fact the new aircraft had to be nuclear-capable. Problem was, security requirements around nuclear weapons in 1947, especially in the development of weapons was so tight that he could obtain no specifics on the nuclear payload the Douglas entry was planned to carry.
Part of the reason for the extreme secrecy was the number of nuclear weapons in the US inventory – a grand total of 13 in 1947. These weapons were the Mk III, a plutonium-fission design that was essentially a production version of “Fat Man” which was dropped on Nagasaki. The Mk III was a bulky design, weighing in at 10,800 lbs, and measuring 12 ft long with a 60-inch diameter. Even though the “physics package” or plutonium core of the weapon was about the size of a grapefruit, the core, tamper and high explosives added considerable heft to the weapon.
Heinemann was convinced of a couple of things, chief of which was that the United States would never be built and, more importantly, that current technology would see a reduction in the size of nuclear weapons. While discussing the design of the plane with a Sandia Labs (weapons development lab) representative, Heinemann allowed as how a reduced size weapon should be thirty-two inches in diameter vice the current 5 foot diameter. Why 32-inches? It just happened to be the diameter set on his compass as he worked on another Douglas aircraft, the F4D. Unbeknownst to Heinemann, the nuclear weapons labs were working on new designs, moving towards designs that were thirty-two inches in diameter. The net effect of this was an aircraft, the A3D that would be both nuclear capable and able to operate off the Midway-class carriers, the largest in the US inventory at the time.
Douglas was awarded a two prototype contract for the XA3D-1 in March 1949, and first flight came three and one-half years later. Like other jet aircraft of the period, the engines proved problematic and the troubled XJ40 engines were replaced by more powerful Pratt & Whitney J57s (9,700lb s.t. vs 7,000lb s.t.). The A3D Skywarrior was Big – 76 ft long with a wingspan of 72 ft and weighing, fully loaded 82,000 lb for the definitive AD3-2 (A-3B variant). With wings spread, one Whale occupied the area of four AD-2’s with their wings folded, a significant chunk of real estate on an already tight carrier deck. More importantly, it had a payload of 12,000 lb – allowing carriage ranging from 12 x 500 lb Mk 82 conventional bombs up to 1 x 7.600lb Mk15 nuclear weapon.
The Mk15, first produced in 1955 and deployed beginning in 1956, was a staged weapon (Teller-Ulam design), using radiation implosion from a fission nuclear primary to implode a secondary stage and a yield of 3.8Mt. Unlike more modern thermonuclear bombs, the Mark 15 used a secondary which was primarily HEU (highly enriched uranium), which generated most of its energy from nuclear fission reactions once the primary imploded it. There was a thermonuclear core which underwent fusion reactions, but most of the energy came from the HEU fissioning. The HEU fission was enhanced by fusion stage neutrons, but would have generated a very significant fission yield by itself. Incidentally, the diameter of the Mk15 was 35 inches.
From the start, the operating order for the A3 would be different from the AJ Savage – it would deploy as an integrated part of the carrier’s airwing. No offloading to Port Lyautey, Morocco. VAH-1 was stood-up to take the Whale to sea. Manned by a collection of carrier and patrol plane pilots, the “Smoking Tigers” received the last of their 12 aircraft and deployed in November 1956 for the Suez Crisis. Since 12 A3D’s on one carrier would be rather overwhelming, the squadron was split with six each going to the new supercarriers – the USS Forrestal (CV-59) and USS Saratoga (CV-60). The successful completion of that short deployment led to a full squadron deployment aboard Forrestal in 1957. Although it presented challenges to the deck crews in spotting and placement on the catapult and proved to be a demanding aircraft in the groove (neutral to unstable in pitch and airspeed that was difficult to control in the landing configuration), the first full deployment by the A3D was still a major success. Proving in particular its night/all-weather nuclear delivery capabilities to Navy and NATO leaders, the pairing of the A3D and the Forrestal-class carrier looked to ensure the longevity of the carrier, a not inconsiderable feat in the face of a determined assault from the Air Force, especially from SAC.
Unfortunately, subsequent deployments were increasingly less successful leading to much concern and criticism in the corridors of naval aviation leadership, particularly from 6th Fleet. Eventually, it reached a pitch where serious review and correction was required. Tapped for this job was CAPT J.D. Ramage. As head of the heavy attack wing, Ramage set about correcting deficiencies in pilot and bombardier/navigator training and experience and community morale.
The Whale continued to evolve in capabilities and employment. It would be deployed on the smaller Essex-class carriers as well as continuing to deploy on Forrestal and later, Kitty Hawk and larger CVs and CVNs. Photo-reconnaissance, in-flight refueling packages and electronic reconnaissance versions would follow. In 1967 the bombing equipment was removed, and modifications made to the nose that led to the variant that would see service well into the 1990s (1987 would be the last shipboard ops).
Specifications (A3D-2/A-3B Skywarrior)
- Crew: 3
- Length: 76 ft 4 in (23.27 m)
- Wingspan: 72 ft 6 in (22.1 m)
- Height: 22 ft 9.5 in (6.95 m)
- Wing area: 812 ft² (75.4 m²)
- Empty weight: 39,400 lb (17,900 kg)
- Loaded weight: 70,000 lb (31,750 kg)
- Max takeoff weight: 82,000 lb (37,200 kg)
- Powerplant: 2× Pratt & Whitney J57-P-10 turbojets, 10,500 lbf (46.7 kN) each
- Maximum speed: 530 knots (610 mph, 980 km/h)
- Cruise speed: 450 knots (520 mph, 840 km/h)
- Range: 1,325 mi (2,130 km)
- Service ceiling: 41,000 ft (12,500 m)
- Rate of climb: ft/min (m/s)
- Wing loading: 86.2 lb/ft² (421 kg/m²)
- Thrust/weight: 0.30
- Guns: 2× 20 mm (0.787 in) cannon in tail turret
- Bombs: 12,000 lb (5,400 kg) of free-fall bombs, including any combination of
- 12× 500 lb (230 kg) Mark 82 bombs or
- 6× 1,000 lb (450 kg) Mark 83 bombs or
- 1,600 lb armor-piercing bombs or
- 500 lb Mark 50 bombs or
- 1,000 lb Mark 36 bombs or
- 2,000 lb Mark 25 mines or
- 1× Mark 15 free-fall nuclear weapon
Miller, Jerry. Nuclear Weapons and Aircraft Carriers: How The Bomb Saved Naval Aviation. Smithsonian Institute Press, 2001.
Swanborough, Gordon and Bowers, Peter M, United States Navy Aircraft since 1911. Naval Institute Press, 1990.
Cochran, Thomas; Arkin, William and Hoenig, Milton M. Nuclear Weapons Databook: Volume 1, U.S. Nuclear Forces and Capabilties. Ballinger Publishing, 1984.