Another trainer prototype, the R.S.3 Desford, was built in 1945.
World War 2
Reid & Sigrist Ltd
Reid & Sigrist Ltd was an instrument manufacturer which opened an aircraft department in 1939 and built a twin-engined advanced trainer popularly known as the Snargasher, of which only a prototype was built. Subcontract work during Second World War included production of Boulton-Paul Defiant two-seat fighters and modification of B-25 Mitchells for the RAF. Another trainer prototype, the R.S.3 Desford, was built in 1945.
Reggiane sa
Built Caproni aircraft during First World War, but closed its aircraft department after the war. Resumed aircraft manufacture in mid-1930s, producing the Ca.405 Procellaria high-performance twin-engine bomber in 1937. Re 2000 Falco I fighter appeared in 1940 with Fiat radial engine, and other versions followed. By 1946 the company had ceased aircraft manufacture and was building railway coaches.
Rearwin Skyranger / Commonwealth 185 / Skyranger

Rearwin Aircraft and Engines introduced the Skyranger in 1940 as a side-by-side two-seat cabin monoplane. Designed by Gene Salvay and George A. Stark, the Skyanger was first flown on 9 April 1940, given Aircraft Type Certificate #729 in 1940.
This aircraft was first produced in four versions: the 175 with a 75-hp Continental, the 180 with an 80-hp Continental, the 180F with a 80-hp Franklin, and the 190F powered by a 90-hp Franklin engine. Seating two people side-by-side, it featured a fabric-covered steel tube fuselage and wooden wing and it sold for about $3000. It had a conventional landing gear with a tailwheel.
About 85 were built by 1941. The Skyranger was the last design of Rearwin Aircraft. Production stopped in 1942 because of the war effort.
In 1942 the Rearwin Airplane Company was purchased by Commonwealth Aircraft of Kansas City, Missouri. In 1943 the company was reorganized as the Commonwealth Aircraft Corp. The Commonwealth Skyranger 185, with its Continental C-85-12 engine, new from the factory on Long Island was about $3,000 in early 1946.

In 1946 Commonwealth re-established the construction of the Skyranger at their Valley Stream plant for just one year. By November of 1946, production of the Skyranger stopped due to market pressures. It had many minor modifications but was essentially the same aircraft. The Skyranger 185 is fabric covered. The fuselage is welded steel tubing, and the wing has wood spars and ribs. A full electrical system was standard, and the aircraft has a large baggage compartment, and wing slots which give better aileron control at low speeds. Two 12.5-gal. wing tanks were standard, 18-gal. tanks were an option. As the anticipated post-war boom in civil aviation had not then started, Commonwealth went bankrupt in 1947, after 275 Skyrangers were built by Commonwealth.

Serial numbers in the 1500s were built by Rearwin. Serial numbers in the 1600s are Commonwealth 185 Skyrangers.
Skyranger 165
Engine: Continental, 65 hp
Wing Span: 34 ft
Length: 21 ft, 9 in
Height: 6 ft, 7 in
Wheel Tread: 74 in
Wing Area: 164.6 sq ft
Wing Loading: 8.2 lbs/sq ft
Power Loading: 20.77 lbs/hp
Empty Weight: 760 lbs
Useful Load: 590 lbs
Gross Weight: 1350 lbs
Baggage and Extra Equipment: 100 lbs
Fuel Capacity: 24 USgal
Fuel Consumption: 4 USgal/hr
Maximum Speed: 105 mph
Cruising Speed: 95 mph
Landing Speed: 38 mph
Cruising Range: 500 miles
Service Ceiling: 12,000 ft
Rate of Climb: 550 ft/min
Skyranger 175
Engine: Continental, 75 hp
Wing Span: 34 ft
Length: 21 ft, 9 in
Height: 6 ft, 7 in
Wheel Tread: 74 in
Wing Area: 164.6 sq ft
Wing Loading: 8.2 lbs/sq ft
Power Loading: 18 lbs/hp
Empty Weight: 760 lbs
Useful Load: 590 lbs
Gross Weight: 1350 lbs
Baggage and Extra Equipment: 100lbs
Fuel Capacity: 24 USgal
Fuel Consumption: 4.6 USgal/hr
Maximum Speed: 110 mph
Cruising Speed: 100 mph
Landing Speed: 38 mph
Cruising Range: 500 miles
Service Ceiling: 14,000 ft
Rate of Climb: 625 ft/min
Type Certificate: 729
Skyranger 180
Engine: Continental, 80 hp
Empty weight: 910 lb
MAUW: 1450 lb
Fuel capacity: 48 USG
Top speed: 114 mph
Cruise speed: 103 mph
Stall: 40 mph
Initial ROC: 650 fpm
Range: 500 miles
Ceiling: 14,000 ft
Seats: 2
Type Certificate: amendment to 729
Skyranger 180F
Engine: Franklin 4AC-176-F3
Type Certificate: amendment to 729
Skyranger 185
Engine: Continental C-185-12, 85 hp (63 kW)
Wing Span: 34 ft
Length: 21 ft, 9 in
Height: 6 ft, 7 in
Wheel Tread: 74 in
Wing Area: 164.6 sq ft
Wing Loading: 8.81 lbs/sq ft
Power Loading: 17.06 lbs/hp
Gross weight: 1,350 lb / 612 kg
Fuel Capacity: 30 USgal
Fuel Consumption: 5 USgal/hr
Endurance: 5 hours
Maximum Speed: 114 mph
Cruising Speed: 103 mph
Landing Speed: 38 mph
Cruising Range: 600 miles
Service Ceiling: 14,000 feet
Rate of Climb: 650 ft/min
Crew: 1
Capacity: 2
Skyranger 190F
Engine: Franklin 4AC-199-E3, 90 hp
Type Certificate: amendment to 729
Rearwin

Rearwin Airplanes was founded by Raymond Andrew (“Rae”) Rearwin in 1928, at Salina, KS.
Following Charles Lindbergh’s historic transatlantic flight in 1927, the world’s fascination with aviation grew significantly. Moreover, the Air Commerce Act of 1926 established the government certification program of pilots and aircraft that gave the fledgling industry safety and legitimacy.
Rearwin produced Junior two-seat light monoplane in 1931, followed by Speedster with American Cirrus engine.
Employing his two sons, Royce and Ken, the small company designed and built over 400 airplanes, including instrument trainers and gliders, despite the effects of the Great Depression.
Taken over in 1935 by partnership called Rearwin Airplanes. In 1937 bought assets of Le Blond Aircraft Corporation renamed as Ken-Royce motors. 1939: Renamed Rearwin Aircraft & Engines Inc.
Rae Rearwin sold the company to the Empire Ordinance Company in 1942. The company built about 275 more Skyrangers under the Commonwealth name before they closed their doors in 1946.
Ranger V-770

The Ranger V-770 was an American air-cooled inverted Vee aero-engine developed by the Ranger Aircraft Engine Division of the Fairchild Engine & Aircraft Corporation and first run in 1931.
In 1931, the V-770 design was put to paper, based on the Ranger 6-440 series of inline air-cooled engines, and test flown in the Vought XSO2U-1 Scout. In 1938 it was tested in the Curtiss SO3C Seamew and found to be unreliable with a tendency to overheat in low-speed flight. By 1941 a more developed V-770 was installed in the Fairchild XAT-14 Gunner prototype and found satisfactory for the production Fairchild AT-21 Gunner gunnery school aircraft.
Produced from 1941 to 1945, the V-770 featured a two-piece aluminum alloy crankcase, steel barreled cylinders with integral aluminum alloy fins and aluminum alloy heads. The V-770 was one of very few V-type, in-line, air-cooled engines to reach production. The engine was used in a relatively small number of Army Air Forces aircraft, among them the Fairchild AT-21 twin-engine trainer of which approximately 175 were built, and in the two Bell XP-77s.
By 1944, the unit cost was US$11,000
Variants:
V-770-4
Installed in the Vought XSO2U-1 Scout
V-770-6
Installed in the XAT-14 Gunner prototype, intended for the Ryan SOR-1 Scout
V-770-7
Installed in the Bell XP-77 light-weight fighter prototype
V-770-8
Installed in the Curtiss SO3C Seamew Scout.
V-770-9
Installed in the XAT-6E Texan prototype.
V-770-11
Installed in the Fairchild AT-21 Gunner.
V-770-15
Installed in the Fairchild AT-21 Gunner.
SGV-770C-1
Tested in the Curtiss XF6C-7 Hawk Fighter-Bomber at 350 hp.
SGV-770D-5
Developed for post-war commercial use, 700 hp (kW) at 3,600 RPM, weight 870 lb (395 kg), height 31.11 in (790 mm), length 74.92 in (1,900 mm), width 33.28 in (846 mm)
Applications:
Bell XP-77
Curtiss SO3C
Edo OSE
Fairchild AT-21
Fairchild BQ-3
Ikarus 214D
Vought XSO2U
Specifications:
SGV-770C-1
Type: 12-cylinder inverted Vee piston engine
Bore: 4 in (101.6 mm)
Stroke: 5 1⁄8 in (130.2 mm)
Displacement: 773 in3 (12.6 L)
Length: 62 in (1,574.8 mm)
Width: 28 in (711.2 mm)
Height: 32.2 in (817.88 mm)
Dry weight: 730 lb (331 kg)
Valvetrain: Two overhead camshafts, one per cylinder bank, gear driven
Supercharger: Single-Speed, Single-Stage, produced 45 inches of mercury (1.5 bar, 7.5 psi) at take-off
Fuel system: Holley non-icing carburetor
Fuel type: 87 octane petrol
Oil system: Full pressure type
Cooling system: Air-cooled
Power output: 520 hp at 3,150 rpm (387.7 kW)
Specific power: 0.673 hp/in3
Compression ratio: 6.5:1
Power-to-weight ratio: 0.71 hp/lb
Ranger Engines / Fairchild Engines
The Ranger Engines Division (also Ranger Aircraft Engine Division) of the Fairchild Engine & Aircraft Corporation was an American aircraft engine company. It was known as the Fairchild Engine Division after World War II.
Panstwowe Zaklady Lotnicze / PZL
Founded January 1928 as Poland’s National Aircraft Establishment, built the P.1 single-seat fighter monoplane with Hispano-Suiza engine in 1929-1930, and subsequently the P.11 single-seat fighter and P.19 cabin monoplane. The PZL Los medium bomber of 1937 was followed by the Wilk twin-engined fighter, Sum light bomber and Mewa reconnaissance monoplane by the beginning of Second World War. Factories at Warsaw- Okecie (original) and Mielec, latter used by occupying Germans as forced-labour Heinkel factory 1940-44.
Under political reorganization in 1956, the Polish aircraft industry was revived with production of Soviet aircraft and some indigenous types. In foreign markets most Polish aircraft subsequently appeared under the PZL title, such as the PZL-101 Gawron and PZL-104 Wilga utility aircraft of 1960 and 1962 respectively, the first being a development of the Yak-12. The Gawron was used extensively as an agricultural aircraft, along with the PZL-built An-2 biplane, but later purpose-built dusters and sprayers were built. PZL types are produced under three separate organizations: PZL “Warszawa-Okecie” SA, WSK “PZL-Mielec” SA, and PZL-Swidnik SA.
Prudden-San Diego Airplane Co / Solar Aircraft Co
The Prudden-San Diego Airplane Company was founded in 1927 by George Prudden and seven San Diego area businessmen. Due to differences in management philosophy between Prudden and his investors, Prudden left the company in November 1928.
1929:
1212 Juniper Ave,
San Diego CA,.
USA
Became the Solar Aircraft Company in March 1929.
Later, Prudden developed the Prudden-Whitehead monoplane with the Atlanta Aircraft Corporation. While in Atlanta, Prudden helped develop Candler Field, Atlanta.
The Solar MS-1 was a prototype all-metal sesquiplane airliner built in 1930 at Lindbergh Field, San Diego, California. Due to the Great Depression in 1929, the company was unable to market the aircraft and made only three airplanes. Solar would never build another aircraft after the MS-1, turning to saucepans to survive the depression, and later stainless-steel exhaust shrouds.
During this period, they won a number of contracts to produce jet engine components. Convinced that the gas turbine was the prime mover of the future, the company invested heavily in the development of small turbines.
The company was reincorporated in 1937 as the Solar Aircraft Company, dropping the “Ltd” from its name. By 1939, Solar Aircraft Company had a work force of 229. Military orders during World War II led to rapid expansion and by the end of the war the company had a workforce of 5,000, largely part of a massive effort to build more than 300,000 exhaust manifolds for U.S. airplanes.
Business dropped considerably after World War II and the management developed a plan to diversify into producing other stainless steel products including caskets, frying pans, bulk milk containers and even redwood furniture; immediately after World War II, the company also produced the Solar Midget race car. Solar’s expertise in hard-to-manufacture parts able to withstand high-temperatures led to contracts to produce jet engine components. Solar Aircraft began to design and manufacture completed turbine engines for the United States military for applications such as auxiliary power units, fuselages, and rocket engine components of guided missiles.
Solar Aircraft Company’s expertise in high-temperature metallurgy led to work producing components for some of the first US jet engines, including the General Electric I-40 and a contract from the US Navy to build an afterburner for the Westinghouse J34. Solar Aircraft Company also won contracts for the Allison J33, Allison J35, Avro Canada Orenda, and Bristol Olympus. It was during this time that one of its engineers, Wendell Reed, developed the pneumatic engine microjet controller, for which he won the Wright Brothers Medal in 1955 and which became widely used for gas turbines, afterburners, and ramjets.
Solar Aircraft Company’s work in the jet engine field convinced the company’s president, Edmund Price, that the turbine would be the main prime mover in the future. Solar Aircraft Company assembled a team under the direction of Paul Pitt in 1946 and started developing a small 80 horsepower (60 kW) axial-flow turbine as an auxiliary power unit for the US Army Air Force’s Convair B-36 strategic bomber. The Army eventually cancelled this contract, but Solar Aircraft Company soon won a contract from the US Navy in 1947 for a 250 kW system to provide emergency power on ships. First running in 1949, the T-400 would go on to provide power on minesweepers and landing craft.
In 1947, Leon Wosika and Eric Balje set up a second design line and developed a centrifugal-flow system that was much more compact than Solar’s previous designs. Originally known as the MPM-45, the unit was delivered as the 45 horsepower (34 kW) “Mars”. The Navy purchased the Mars to power portable fire-fighting pumps on ships and gave it the designation T41. In 1956, the Navy turned to Solar to provide a slightly larger design to power a small helicopter, the Gyrodyne XRON-1. Solar Aircraft Company responded by developing a slightly larger version of the Mars, the 55 horsepower (41 kW) “Titan”, which the Navy designated the T62. When the Navy abandoned development of Gyrodyne’s XRON helicopter, Solar Aircraft Company adapted the Titan for service as an auxiliary power unit. Deliveries of this auxiliary power unit started in 1962.
Solar did win the contract to provide the APU for the first 632 KC-135A tankers for the Strategic Air Command.
In the late 1950s, the Navy once again turned to Solar, this time for a larger 750-kilowatt (1,010 hp) unit that would be used as an engine in a high-speed boat. The result was the axial-flow “Saturn” engine, which entered production in 1960. Solar started marketing the Saturn to industrial users needing a 1,000-horsepower (750 kW) unit for any role, and it went on to become the world’s most widely used industrial gas turbine with some 4800 units in 80 countries.
During the next decade, the Solar Division introduced a number of new designs, both larger and smaller than the Saturn. The Centaur, which first entered service in 1968, supplied 2,700 horsepower (2,000 kW), while the modern versions supply 4,700 horsepower (3,500 kW). In 1973, Solar exited the aviation industry to concentrate its resources on industrial gas turbines.
The turbine never came to be the main prime mover, but Solar’s expertise in small turbines found a number of niche roles. The company was purchased by International Harvester Company in early 1960, becoming the Solar Division of International Harvester in 1963. In 1973, the Solar Division exited the aerospace industry to focus solely on industrial turbines. In 1975, the development and manufacture of the Solar Division’s radial engines was moved into a newly formed Radial Engines Group, renamed the Turbomach Division in 1980.
In 1977, the Solar Division introduced a larger version of the Centaur, the 10,600 horsepower (7,900 kW) Mars, re-using the name from the earlier smaller engine.
Solar Turbines Incorporated became a wholly owned subsidiary of Caterpillar Tractor Co. after Caterpillar purchased the assets of the Solar Division and the Turbomach division from International Harvester on 31 May 1981. The newly acquired assets were organized as a wholly owned subsidiary of Caterpillar Tractor Co. named Solar Turbines Incorporated.
After the purchase, Caterpillar assigned development and manufacturing of the Caterpillar Model 5600 to Solar Turbines. The 5600 was originally developed by The Boeing Company as the Boeing 551/553 series, which Caterpillar had purchased when Boeing decided to exit the gas turbine business in 1966.
In 1985, Caterpillar sold the Turbomach Division to Sundstrand Corporation (now Collins Aerospace), exiting the Centrifugal gas turbine engine business.
Solar Turbines Incorporated continued to introduce new versions of their axial-flow industrial engines throughout the 1980s and 90s, often re-using older names instead of introducing new names.
In 2004 Caterpillar acquired Swiss company Turbomach S.A. which had long been a packager of industrial turbines from Solar, Rolls-Royce, and Trent.
Solar has sold more than 15,000 gas turbine systems, with a combined operating history of over 2 billion hours of use, equivalent to over 100,000 years.
Proctor Coogee
Designed and built by Tom Proctor in Australia during 1940-41, The Coogee is essentially a scaled up Hutter 17 hlider.
Registered VH-GFD, Tom Proctor made about 200 short flights in it from 1942 to 1945 and it was then sold to the Victorian Motorless Flight Group. In 1956 ownership changed to the Geelong Gliding Club and subsequently in 1963 it was acquired by E.J. Williams and F.G. Wyer who undertook a thorough overhaul and a complete re fabric of it.
It was then sold to G.C. Curtis, F.O. Connell and R.T. Harris in 1966 who retired it from service 1967 after a total of 3,851 flights and 415 Hours.
The Coogee was donated to a museum by the C. Curtis/G. Downs estate, and restored to display condition.