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Stroukoff YC-134 Pantobase
 
Stouk-C134-01
YC-134 52-1627 at Moffett Field, June 1959
 
The Stroukoff YC-134, designed in 1956, was based heavily on the Fairchild C-123 Provider. The United States military contracted with Stroukoff Aircraft Corporation to develop an improved version of the aircraft, combining features that the company had developed for the YC-123D and YC-123E.
 
The product of a US Air Force contract in 1956, a single C-123B from the -CN production block (serial 52-1627) was modified by Stroukoff Aircraft to become the YC-134. This aircraft was heavily modified with the following new features:
 
New Engines: The YC-134 was equipped with two 3,500 hp (2,600 kW) Wright Turbo Compound R3350-89A radial engines, turning four-blade, thirteen foot Aeroproducts constant-speed fully feathering propellers.
 
A new thickened wing. In the root of the wing they installed two turbocompressors with 400 hp each
 
Improved Control Surfaces: The YC-134's horizontal stabilizers were given endplates to improve directional stability.
 
Improved landing gear: While the nosewheel from the C-123B was retained, both main gears were given a third wheel to improve weight distribution.
 
Fuel was no longer housed in the rear of the engine nacelles, but in an expanded center-wing fuel tank. In addition, two plumbed hardpoints for 550-gallon drop tanks were also added to each wing.
 
Stouk-C134-02
 
Stroukoff's BLC and Pantobase: the YC-134 was fitted with Stroukoff's own BLC and all three aircraft had they been delivered were to have been fitted with the Pantobase equipment designed for the YC-123E.
 
The features gave an empty weight increase over the C-123B from 31,058 lb (14,088 kg) to 37,965 lb (17,221 kg), and a maximum loaded weight increase from 60,000 lb (27,000 kg) to 74,700 lb (33,900 kg). The aircraft's cruising speed was 219 mph (352 km/h), compared to the C-123B's 190 mph (310 km/h), and the YC-134 had a 1,600-mile (2,600 km) range with a 24,000 lb (11,000 kg) payload. The BLC allowed the YC-134's take-off distance to decrease from 1,850 feet (560 m) to 750 feet (230 m), very similar to that of the YC-123D.
 
The aircraft for the first time rose into air on 19 December, 1956, on the tests were obtained good results, and servicemen ordered two additional machines. On them they installed the modernized boundary-layer control system with one more powerful compressor and "pantobase". The YC-134 gained the designation "Pantobase" after hydro-skis were added. The YC-134 demonstrated following: takeoff on the earth - 244 m, on the snow and the water - 458 m; path on the earth - 320 m, on the snow - 305 m, on the water - 228 m. In the beginning of 1958 all three YC-134 were transferred to the Air Force.
The U.S. Air Force, however, deemed that the YC-134 did not offer substantial improvement over the C-123, nor did it have a requirement for a piston-engined amphibious assault transport, and decided to purchase the Lockheed C-130 Hercules.
 
Stouk-C134-03
YC-134A 55-4031) with Pantobase system for amphibious operations

YC-134-SA
Engine: 2 × Wright R-3350-89A, 3,500 hp
Payload: 24,000 lb
Empty weight: 37,965 lb (17,221 kg)
Max. takeoff weight: 74,700 (33,900 kg)
Cruise speed: 219 mph (352 km/h)
Range: 1,600 miles (2,600 km) with 24,000 lb (11,000 kg) payload
Take-off distance: 750 feet (230 m)
 
 
 
 


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