Category Archives: Fighterbomber

Fighterbomber

Douglas BTD-1 Destroyer (Planet, Resin)

TYPE: Carrier-borne scout/dive bomber

ACCOMMODATION: Pilot only

POWER PLANT: One Wright R-3350-14 Cyclone 18, rated at 2,300 hp

PERFORMANCE:  334 mph at 16,100 ft

COMMENT: The Douglas BTD Destroyer was an American dive/torpedo bomber developed for the United States Navy during World War II. A small number had been delivered before the end of the war, but none saw combat.
On June 1941, the United States Navy placed an order with the Dougla Aircraft Company for two prototypes of a new two-seat dive bomber to replace both the Douglas SBD Dauntless and the new Curtiss SB2C Helldiver, designated XSB2D-1. The resulting aircraft, designed by a team led by Ed Heinemann, was a large single-engined mid-winged monoplane. It had a laminar flow gull-wing, and unusually for a carrier-based aircraft of the time, a tricycle undercarriage. It was fitted with a bomb bay and underwing racks for up to 4,200 lb of bombs or one torpedo (typically the Marl 13), while defensive armament consisted of two wing-mounted 0.79 in cannon and two remote-controlled turrets, each with two .50 in machine guns.
The prototype first flew on April 1943, demonstrating good performance, being faster than the Dauntless and capable of carrying more bombload, but it was heavier and more complex. The U.S. Navy had made a request for a new torpedo bomber developed from the XSB2D-1. Douglas reworked the XSB2D-1 by removing the turrets and second crewman, while adding more fuel and armor, while wing racks could carry not just one but two torpedoes, producing the BTD-1 Destroyer. The orders for the SB2D-1 were converted to the BTD-1, with the first BTD-1 flying on March 1944. The BTD-1 was heavier than the XS2BD-1 and had poorer performance. Ed Heinemann asked for cancelling of the BTD-1.
The first production BTD-1s were completed in June 1944. By the time Japan surrendered in August 1945, only 28 aircraft had been delivered, and production was cancelled due to performance, along with other aircraft types that had been designed from the start as single-seaters, such as the Martin AM Mauler. None saw combat action. In any event, Heinemann and his team were already working on developing the single-seat BT2D that became the Douglas A-1 Skyraider (Ref.: 24).

Douglas XA2D-1 Skyshark (Anigrand, Resin)

TYPE: Carrier-borne attack aircraft

ACCOMMODATION: Pilot only

POWER PLANT: Allison XT40-A2 coupled turboprop engine, rated at 5,100 h.p., driving two contra-rotating three-bladed propellers,

PERFORMANCE: 492 mph at 40.000 ft

COMMENT: The Douglas A2D Skyshark was an American carrier-borne turbopropeller-powered attack aircraft built by the Douglas Aircraft Company for the US Navy. The program was substantially delayed by engine reliability problems, and was canceled because more promising turbojet attack aircraft had entered development and the smaller escort carriers the A2D was intended to utilize were being phased out.
On June 1945, the Bureau of Aeronautics (BuAer) asked Douglas Aircraft for a turbine-powered, propeller-driven aircraft. Three proposals were put forth in the next year and a half: the D-557A, to use two General Electric TG-100s (T31s) in wing nacelles; the D-557B, the same engine, with counter-rotating propellers; and the D-557C, to use the Westinghouse 25D. These were canceled due to engine development difficulties, but BuAer continued to seek an answer to the high fuel-consumption of the turbojet powered aircraft.
On June 1947 Douglas received the Navy’s letter of intent for a carrier-based turboprop-powered aircraft. The need to operate from Casablanca-class escort carriers dictated the use of a turboprop instead of turbojet power.
While it resembled the in service Douglas AD Skyraider, the A2D was different in a number of unseen ways. The 5,100 hp rated Allison XT-40-A-2 had more than double the horsepower of the Skyraider’s Wright R-3350 Cyclone air-cooled piston engine. The XT40 installation on the Skyshark used contra-rotating propellers to harness all the available power. Wing root thickness decreased, from 17% to 12%, while both the height of the tail and its area grew.
Engine-development problems delayed the first flight until May 1950 and on December 1950, the first prototype crashed while landing approach killing the pilot. Investigation found the starboard power section of the coupled Allison XT-40-A-2 turboprop engine had failed and did not declutch, allowing the Skyshark to fly on the power of the opposite section, nor did the propellers feather. As the wings’ lift disappeared, a fatal sink rate was induced. Additional instrumentation and an automatic decoupler was added to the second prototype, but by the time it was ready to fly on April 1952, sixteen months had passed, and with all-jet designs being developed, the A2D program was essentially dead. Total flight time on the lost airframe was barely 20 hours.
Allison failed to deliver a “production” engine until 1953, and by the summer of 1954, the new Douglas A4D Skyhawk pure turbojet-powered ground attacker was ready to fly. The escort carriers were being mothballed, and time had run out for the troubled A2D program.
Due largely to the failure of the T40 program to produce a reliable engine, the Skyshark never entered operational service. Twelve Douglas A2D Skysharks were built, two prototypes and ten preproduction aircraft. Most were scrapped or destroyed in accidents, and only one has survived (Ref.: 24).

Goodyear FG-4 Corsair, VMF-111 (Hasegawa)

TYPE: Carrier-based fighter-bomber

ACCOMMODATION: Pilot only

POWER PLANT: Pratt 6 Whitney R-2800-18W Double Wasp, rated at 2,100 h.p.

PERFORMANCE: 390 m.p.h. at 24,000 ft