History of the Curtis-Wright C-46 Commando

The U.S. Air Force used the C-46 Commando series as the primary mode of transportation in the Pacific Theater during World War II. The system was originally intended to replace the Douglas series DC-3 transport aircraft and first appeared in March 1940 as a prototype for the twin-rudder CW-20T.

Design specifications call for the Commando to have a pressurized pod for up to 36 combat-ready troops, longer range and superior cruising speed than anything available to the USAAF (United States Army Air Force).

The CW-20T prototype later evolved into the CW-20A, which featured an improved empennage in the form of a more recognizable single rudder assembly. Subsequent development focused on the needs of the US Army Air Corps, which tested the CW-20A under the designation C-55, and then ordered a production version of the model, now designated CW-20B.

CW-20B renamed to more familiar C-46 designation. The final experimental model was provided for up to 45 combat-ready troops and was equipped with two Pratt & Whitney R-2800-51 radial engines.

The C-46 served in the Pacific Theater under the simple designation "C-46" - almost exclusively there until around March 1945, and commandos were also seen throughout the European Theater. From its initial acceptance into U.S.

Air Force service, the C-46 system has gradually become the heaviest aircraft in the service, earning its reputation as a true warrior workhorse, transporting troops and cargo on and off the battlefield.

There are many variants of the C-46 Commando. The U.S. Navy uses the R5C designation for its own Commando version, of which 160 R5C-1 variants will be delivered to the U.S. Marine Corps. Specialized utility and troop models will be manufactured from hundreds to thousands.

The C-46A Commando itself can carry up to 50 infantrymen and load and unload cargo through a large cargo door on the port side of the aircraft.

The C-46 was officially retired in 1968, replaced by the equally effective C-130 transport series.

Specification

Basic

Year:
1941
Status:
Active Limited Service
Staff:
4

Production

[3,181 units]:
Curtis Wright - USA

Roles

- Traffic

Dimensions

Length:

23.3m

Width:

23.94m

Height:

6.63m

Weight

Curb Weight:

14,700 kg

MTOW:

20,415 kg

(difference: +12,599 pt)

Performance

2 x Pratt & Whitney R-2800-51 "Twin Wasps" 18-cylinder air-cooled radial piston engines, each producing 2,000 hp and driving a four-blade propeller unit.

Performance

Maximum Speed:

270 mph (435 km/h; 235 knots)

Service Limit:

27,559 ft (8,400 m; 5.22 mi)

Maximum range:

3,150 miles (5,070 km; 2,738 nautical miles)

Rate of climb:

358 m/min

Armor

No.

Changes

CW-20T - Dual Fin Prototype

CW-20A - Rebuilt from CW-20T prototype model; revised tail now features a single tail assembly; flattened tail halves.

C-55 - CW-20A designation as assessed by the US Army Air Forces.

CW-20B - A militarized custom production model of the US Army Air Forces CW-20A/C-55 evaluation model; renamed the C-46.

C-46 - Curtiss CW-20B model based on the CW-20B.

C-46A - Improved and final C-46 model; 1,493 produced; equipped with R-2800-51 radial engine; reinforced bottom; accommodation for up to 50 soldiers; large loading gate to port.

XC-46B - Stepped Windshield

XC-46C - became C-46G, then XC-113

C-46D - Improved C-46A; troop transport; two-door model with improved nose assembly.

C-46E - Single-door model; 17 produced.

C-46F - Improved C-46A; commercial traffic; 234 produced.

C-46G - XC-46C models

XC-113 - C-46G model

R5C - United States Navy Model

R5C-1 - United States Marine Corps Model; 160 produced.

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