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The aircraft was built to comply with FAA part 103 rules for ultralight aircraft. The fuselage is constructed of welded aluminum tubing. The cantilever main wing is capable of rotating 90 degrees for storage without removal from the fuselage. The 40 hp engine uses a Valley Engineering Series Three PSRU.
Standard engine is the 50 hp (37 kW) Rotax 503 with the 64 hp (48 kW) Rotax 582 as an option. [6] Phantom I-E Single seat ultralight aircraft with struts in place of cable-bracing and enclosed cockpit with removable doors. Standard engine is the 50 hp (37 kW) Rotax 503 with the 64 hp (48 kW) Rotax 582 as an option. [6] Phantom II
An aircraft engine, often referred to as an aero engine, is the power component of an aircraft propulsion system. Aircraft using power components are referred to as powered flight . [ 1 ] Most aircraft engines are either piston engines or gas turbines , although a few have been rocket powered and in recent years many small UAVs have used ...
The General Electric XA102 is an American adaptive cycle engine demonstrator being developed by General Electric (GE). It is competing with the Pratt & Whitney XA103 as the powerplant for the United States Air Force's sixth generation fighter program, the Next Generation Air Dominance (NGAD).
On 24 December 1985, the U.S. Navy selected Allison's engine for full-scale engine development and production on the U.S. Marine Corps's V-22 Osprey. [5] Before the engine was given its United States military aircraft engine designation of T406, it was known as the Model 501-M80C. [6]
Wright Aeronautical (1919–1929) was an American aircraft manufacturer headquartered in Paterson, New Jersey. [1] It was the successor corporation to Wright-Martin. [1] It built aircraft and was a supplier of aircraft engines to other builders in the golden age of aviation. [1]
The Lawrance Aero Engine Company was founded in 1917. [2] After the end of World War I, the Lawrance engineers worked with both the Army and the Navy in developing their L-1 into a nine-cylinder radial engine, which became the 200 hp Lawrance J-1. It was the best American air-cooled engine at the time, and passed its 50-hour test in 1922. [3]
In 1929, the company introduced its first aircraft engine, [3] a seven-cylinder radial designated as the A-70, with a displacement of 543.91 cu in (8.91L) that produced 170 hp (127 kW). In August 1929, the Continental Motors Company formed the Continental Aircraft Engine Company as a subsidiary to develop and produce its aircraft engines. [4]