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The Short SC.7 Skyvan (nicknamed the "Flying Shoebox") [1] is a British 19-seat twin-turboprop aircraft first flown in 1963, that was manufactured by Short Brothers of Belfast, Northern Ireland. Featuring a basic rugged design and STOL capabilities, it was used in small numbers by airlines, and also by some smaller air forces.
In 1937 and 1938, a second civilian aircraft model was introduced, the S-C Sport Coupe, or SC-W with a 145 hp (108 kW) Warner Super Scarab radial engine. The SC-W was a larger three-seater aircraft with a sliding canopy and side-by-side front seating. The prototype SC-M was originally powered by a Menasco C-4 inline engine, however testing ...
Production aircraft powered by a 145hp (108kW) Warner Super Scarab radial engine, 12 built. L-10 United States Army Air Forces designation for one S-C-W impressed into service in 1942, it was disposed of in November 1944. [4] Later Modifications Two SC-Ws exist with a horizontally opposed 6-cylinder Continental engine. One was modified from a ...
USS Alaska recovering a SC-1 in March 1945, during the Iwo Jima operation. The aircraft is awaiting pickup by the ship's crane after taxiing onto a landing mat. A U.S. Navy SC-1 from USS Duluth over Shanghai, China in 1948 An SC-1 Seahawk being hoisted aboard USS Manchester during a deployment to the Mediterranean Sea from in 1947/1948 Seahawk on board USS Birmingham
The engine casing of the early motors is made of an aluminium alloy. On introduction, fuel pellets and wick could be purchased separately, meaning that the system is reusable. [2] Jetex power made a big impact in the late 1940s and early 1950s, allowing new sorts of models, scale and duration, to be designed.
Data from Compact Radial Engines General characteristics Type: Three cylinder, radial two-stroke aircraft engine Bore: 66 mm (2.60 in) Stroke: 42 mm (1.65 in) Displacement: 430 cc (20.75 cu in) Dry weight: 17 kg (37 lb) Components Valvetrain: rotary valve induction Oil system: premixed oil and fuel Cooling system: air cooled Reduction gear: none Performance Power output: 20 hp (15 kW) at 4200 ...
Scaled Composites Model 205, first preliminary design for airlaunch of a booster rocket heavier than 500,000 pounds (230,000 kg) (1991) [2] Scaled Composites Model 206 , second preliminary design for heavy airlaunch (1991) [ 2 ]
Photos of this type show the removal of underslung engine oil coolers typical of the R-1830 engine installation; apparently not needed in the cold polar regions. R4D-5Q R4D-5 for use as special ECM trainer. Redesignated EC-47H in 1962 R4D-5R R4D-5 for use as a personnel transport for 21 passengers and as a trainer aircraft; redesignated TC-47H ...