Here are some 1-144 scale pixel art I had drawn based around AU history and engineering I sometimes mess around with. For those who like their AU and alternate engineering.
Soaring Eagle: The RAAF that Williams Wanted
The following is first of many (I hope) chapters describing an alternate history based around a correction of the poor and often conspiring decisions made in Australia in the 1930s and 40s that significantly reduced the capability of military and civil aviation. While mostly focusing on alternate aviation decisions and effects I will also cover other areas and strategic effects that would be influenced by a change in events. My primary source for this endeavour is the book “Wounded Eagle” by Dr Peter Ewer which charts the history of Australian aviation policy history during this era. It’s an excellent book and based on historical research in Australian and British archives. The most shocking events in my exploration are likely to be those based on actual events. Hopefully I can dish out some fictional comeuppance to those people whose actions in the name of Imperial interests (ie British complacency) resulted in an Australia unable to defend itself in time of need.
Development of the Woomera Bomber
On 27 March 1939 the Lyons Government endorsed the submission by Defence Minister Charles Hawker to contract with CAC for development and eventual production of 180 CA-4 Wirraway Bombers. The new bomber was to provide the RAAF with a high performance anti-ship bomber capable of both torpedo attacks and dive bombing. The new bomber would use Australian built Pratt & Whitney Twin Wasp engines that were common across the RAAF’s new force of American built Curtiss Hawk fighters, Lockheed Australis patrol bombers and Consolidated Condor amphibians. From the back bench of Parliament former minister Robert Menzies was highly critical insisting that production of the British Beaufort bomber would be better suited to Empire defence. With the scandal of his dismissal from Cabinet as part of the Bruce Papers Affair still fresh Menzies was unable to make much leeway with public opinion. His opposition to the Wirraway Bomber would be one of his final public acts before leading the short-lived Empire Party split from the governing United Australia Party.
In May 1939 CAC’s general manager and chief designer Lawrence Wackett presented his Wirraway Bomber design to the Chief of Air Staff Air Vice Marshall Richard Williams for approval. The new design reused much of the Wirraway (itself based on the North American NA-16) including the outer wings and tail. To meet the RAAF’s demanding long range requirement (over 2,000 miles or eight hours cruising at 250 mph) the bomber used a self sealing fuel tank integral with the central wing. Also heavy defensive armament was provided by four rear firing machineguns in two remote control barbettes in the engine pods. Williams having a long history of working with Wackett dating back to the desert campaign in WWI was able to ‘persuade’ Wackett to redesign the aircraft to remove the troublesome not so sealing fuel tank and the un-controllable barbettes. The bomber was to be redesigned and also benefit from feedback from CSIRO’s new wind tunnel which was operational from April 1939.
When re-presented to the RAAF in August the Wirraway Bomber had a longer and sleeker fuselage and several important changes. Without the need for an integral fuel tank the new wings were slimmer and now held the inwards folding main landing gear which was removed from the engine pods. The later were larger and more aerodynamic with each holding a large conventional self sealing fuel tank with oil coolers, exhausts and other engine auxiliary equipment above it. In the centre of the fuselage was the main fuel tank which divided the nose from the tail. The pilot was now seated forward of the wing above the four forward firing Browning .303 machineguns and radios. In front of the pilot was the navigator/bomb aimer who had originally been positioned in the rear fuselage. The navigator was able to carry out all his tasks form the seat as the bomb aiming role was only to support shallow angle dive bombing and his simple sight looked down and forward between his legs. He also had fold away, auxiliary controls to fly the aircraft if the pilot was incapacitated. The most significant change was the defensive armament which now consisted of a tail gunner and four rear firing Brownings in a pod beneath the tail. This configuration was provided by the RAAF’s Australian Technical Mission to America (ATMA) Los Angeles office who copied it from the new Douglas B-23 Dragon bomber.
When the prototype Wirraway Bomber, now christened the Woomera, was ready to fly in March 1940 the RAAF was at war and with a huge demand for bombers to equip the Australian Air Expeditionary Force (AAEF) being deployed to Europe. Flying trials revealed the Woomera was one of the fastest bombers in the world in 1940 being able to reach 330 mph without bombs or a torpedo while using the new high octane fuel. Since the CA-3 Wirraway Fighter project had been cancelled thanks to the ready supply of Curtiss Hawks CAC was able to progress the Woomera through development to production by 1941. Alongside the CA-1 Wirrway advanced trainer and army co-operation aircraft and CA-2 Warrigal basic trainer the CA-4 Woomera drive and torpedo bomber rolled out of the Fisherman’s Bend factory in Melbourne for RAAF service.
By December 1941 150 Woomeras had been delivered equipping the No. 4 Operational Training Unit (Woomera conversion and dive bombing), No. 6 Operational Training Unit (torpedo dropping at Jervis Bay) and No. 6 Squadron recently rushed to Malaya before being qualified on torpedo attacks. Two additional squadrons (Nos. 46 and 47) were forming with the Woomera but had not been brought to full strength or declared operational. The Woomera was soon to face its toughest test with the impending onslaught of the Japanese forces in the Pacific.
CAC CA-4/CA-11 Woomera
General Characteristics
Crew: 3 (pilot, bomb aimer/navigator, rear gunner)
Length: 49 ft 8 in (15.14 m)
Wingspan: 59 ft 2½ in (18.05 m)
Height: 15 ft 2 in (4.62 m)
Wing area: 440 ft² (40.9 m²)
Empty weight: 12,952 lb (5,875 kg)
Max takeoff weight: 23,425 lb (10,647 kg)
Powerplant: 2× Pratt & Whitney R-1830-S3C3-G Twin Wasp 14-cylinder two-row radial engine, 1,200 hp (895 kW) each
Performance
Maximum speed: 332 mph (531 km/h, 295 knots)
Range: 2,000 mi (3,200 km, 1,778 NM) (with 2,000 lb of bombs or torpedo)
Service ceiling: 23,500 ft (7,165 m)
Rate of climb: 2,090 ft/min (10.6 m/s)
Armament
4 × .303” (7.7 mm) Browning machine guns in nose
4 × .303” (7.7 mm) Browning machine guns in rear firing mount
4 × 500 lb (224 kg) bombs or 2 x 1,000 lb (454 kg) bombs or 1 x 1,548 lb (702 kg) Mk 12 18” (45 cm) torpedo under fuselage and 4 × 25 lb (13 kg) bombs under wings