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Shot with the Canon RF 100-500 and 24-70 lenses.

US Civil Registration: N54510

USAF Serial: 44-77575

Curtiss C/N: 32955

  

From Wikipedia:

 

en.wikipedia.org/wiki/Curtiss_C-46_Commando

 

The Curtiss C-46 Commando is a twin-engine transport aircraft derived from the Curtiss CW-20 pressurised high-altitude airliner design. Early press reports used the name 'Condor III' but the Commando name was in use by early 1942 in company publicity. It was used as a military transport during World War II by the United States Army Air Forces and also the U.S. Navy/Marine Corps, which used the designation R5C. The C-46 served in a similar role to its Douglas-built counterpart, the C-47 Skytrain, but it was not as extensively produced as the latter.

 

After World War II, a few surplus C-46 aircraft were briefly used in their originally designated role as passenger airliners, but the glut of surplus C-47s dominated the marketplace and the C-46 was soon relegated to primarily cargo duty. The type continued in U.S. Air Force service in a secondary role until 1968. The C-46 continues in operation as a rugged cargo transport for Arctic and remote locations with its service life extended into the 21st century.

 

The prototype for what would become the C-46, the Curtiss CW-20, was designed in 1937 by George A. Page Jr., the chief aircraft designer at Curtiss-Wright. The CW-20 was a private venture intended to compete with the four-engined Douglas DC-4 and Boeing 307 Stratoliner by the introduction of a new standard in pressurized airliners. The CW-20 had a patented fuselage conventionally referred to as a "figure-eight" (or "double-bubble") which enabled it to better withstand the pressure differential at high altitudes.[6] This was done by having the sides of the fuselage creased at the level of the floor that not only separated the two portions but shared in the stress of each, rather than just supporting itself. The main spar of the wing could pass through the bottom section which was mainly intended for cargo without intruding on the passenger upper compartment. A decision to utilize a twin-engine design instead of a four-engine configuration was considered viable if sufficiently powerful engines were available, allowing for lower operating costs and a less complex structure.

 

Engineering work involved a three-year commitment from the company and incorporated an extensive amount of wind tunnel testing at the California Institute of Technology (Caltech). The resultant design was a large but aerodynamically "sleek" airliner, incorporating the cockpit in a streamlined glazed "dome". The engines featured a unique nacelle tunnel cowl where air was ducted in and expelled through the bottom of the cowl, reducing turbulent airflow and induced drag across the upper wing surface. After a mockup was constructed in 1938, Curtiss-Wright exhibited the innovative project as a display in the 1939 New York World's Fair.

 

The company approached many airlines in order to obtain their requirements for an advanced airliner. No firm orders resulted, although 25 letters of intent were received, sufficient to begin production. The design of a 24–34 passenger airliner proceeded to prototype stage as the CW-20 at the St. Louis, Missouri facility with the initial configuration featuring twin vertical tail surfaces. Powered by two 1,700 hp (1,300 kW) R-2600-C14-BA2 Wright Twin Cyclones, the prototype, registered NX-19436 flew for the first time on 26 March 1940 with test pilot Edmund T. "Eddie" Allen at the controls. After testing, modifications were instituted, including the fitting of a large single tail to improve stability at low speeds.

 

The first prototype was purchased by the United States Army Air Forces (USAAF) to serve as a master for the series and was designated C-55. After military evaluation, the sole example was returned to Curtiss-Wright and subsequently re-sold to the British Overseas Airways Corporation (BOAC). During testing, General Henry H. "Hap" Arnold became interested in the potential of the airliner as a military cargo transport and on 13 September 1940, ordered 46 modified CW-20As as the C-46-CU Commando; the last 21 aircraft in this order were delivered as Model CW-20Bs, called C-46A-1-CU. None of the C-46s purchased by the U.S. military were pressurized and the first 30 delivered to the AAF were sent back to the factory for 53 immediate modifications. The design was then modified to the C-46A configuration, receiving enlarged cargo doors, a strengthened load floor and a convertible cabin that speeded changes in carrying freight and troops. The C-46 was introduced to the public at a ceremony in May 1942, attended by its designer, George A. Page Jr.

 

A total of 200 C-46As in two initial batches were ordered in 1940, although only two were actually delivered by December 7, 1941. At this time, one other important change was made; more powerful 2,000 hp Pratt & Whitney R-2800 Double Wasp engines replaced the two Wright Twin Cyclones. By November 1943, 721 modifications had been made to production models, although many were minor, such as fuel system changes and fewer cabin windows were also adopted. Subsequent military contracts for the C-46A extended the production run to 1,454 examples, 40 of which were destined for the U.S. Marine Corps, to be designated R5C-1. The military model was fitted with double cargo doors, a strengthened floor and a hydraulically operated cargo handling winch; 40 folding seats were the sole passenger accommodation for what was essentially a cargo hauler. Two C-46 were delivered from Higgins Industries Michoud Factory Field in 1942.

 

The final large production-run C-46D arrived in 1944–45, and featured single doors to facilitate paratroop drops; production totaled 1,430 aircraft. Although a one-off XC-46B experimented with a stepped windscreen and uprated powerplants, a small run of 17 C-46Es had many of the same features as the XC-46B along with three-bladed Hamilton-Standard propellers replacing the standard Curtiss-Electric four-bladed units. A last contract for 234 C-46Fs reverted to the earlier cockpit shape but introduced square wingtips. A sole C-46G had the stepped windscreen and square wingtips but the end of the war resulted in the cancellation of any additional orders for the type.

  

Photo by Eric Friedebach

Shot with the Canon RF 100-500 and 24-70 lenses.

All taken within 3 minutes.

Thanks to Kurt Sneddon for showing me the (for me very hard) art of patience to wait for that almost non-existant fraction of a second where less distractios are in the frame, so that the attention will better focus on the subject.

Though not always easy in candid photography, it is something only an experienced photographer could tell.

You may want to check Kurt's community here It's a great place to grow in a non-toxic environment.

Canon R5C with Mamiya 110mm F2.8 lens at F2.8

 

A classic sunrise viewed from Midtown Atlanta.

This RF-8G 146839 served previously with VFP-306 'Peeping Toms' at NAF Washington DC but is now unmarked. The Marines R5C-1 39611 is actually C-46 ex-USAAF 43-47350, which post-WWII had a clandestine career with CAT in China before joining Zantop as N611Z.

 

Both aircraft are displayed outside at the super National Naval Museum at Pensacola, Florida.

Home studio setup with elinchrom lighting using my canon R5c

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