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The Bristol Siddeley Orpheus is a single-spool turbojet developed by Bristol Siddeley for various light fighter/trainer applications such as the Folland Gnat and the Fiat G.91. Later, the Orpheus formed the core of the first Bristol Pegasus vectored thrust turbofan used in the Harrier family.
The Fiat G.91 is a jet fighter aircraft designed and built by the Italian aircraft manufacturer Fiat Aviazione, which later merged into Aeritalia.. The G.91 has its origins in the NATO-organised NBMR-1 competition started in 1953, which sought a light fighter-bomber (officially, the competition was seeking a "Light Weight Strike Fighter") to be adopted as standard equipment across the air ...
A Fiat G.91Y at Ramstein Air Base in 1986. The Fiat (later Aeritalia) G.91Y is an Italian ground-attack and reconnaissance aircraft which first flew in 1966. Although resembling its predecessor, the Fiat G.91, the aircraft was in fact a complete redesign, a major difference being that it was equipped with a new twin-engine configuration, replacing the original single engine.
Bristol Siddeley Engines Ltd (BSEL) was a British aero engine manufacturer. The company was formed in 1959 by a merger of Bristol Aero-Engines Limited and Armstrong Siddeley Motors Limited . In 1961 the company was expanded by the purchase of the de Havilland Engine Company and the engine division of Blackburn Aircraft .
In past decades, appearance packages have also included two-tone paint, pin striping, bumpers painted the same color as the vehicle body, and vinyl roof covers. Sports/performance package: May include engine upgrades, handling upgrades (see below), a more aggressive front spoiler, a rear wing, upgraded brakes, and a limited slip differential.
Hermès stock rose as much as 4.2% in Paris on Friday, pushing the market cap above 300 billion euros for the first time. Shares have jumped 23% this year and about 300% over the past five years ...
The Bristol design was the Type 172 and was to be powered by four or six Bristol engines of 9,000 lbf (40 kN) thrust [7] to the Ministry engine specification TE.1/46. The thrust required of the new engine, then designated B.E.10 (later Olympus), would initially be 9,000 lbf (40 kN) with growth potential to 12,000 lbf (53 kN).
New cadets march during Reception Day at the U.S. Military Academy in West Point, N.Y., on June 27, 2016. Credit - Drew Angerer—Getty Images