Search results
Results from the WOW.Com Content Network
The aircraft is powered by two GE Honda HF120 turbofans, developed with GE Aviation under the GE-Honda partnership. Honda began developing its own small turbofan engine, the HF118, in 1999, leading to the HF120. The HF120 was test-flown on a Cessna Citation CJ1. [78] The engine features a single fan, a two-stage compressor and a two-stage turbine.
The 1963 Learjet 23 was the first light jet. The first large, long-range jet was the Grumman Gulfstream II in 1966. The 25,000 lb (11 t) MTOW British Aerospace 125 first flew on 13 August 1962 as the de Havilland DH.125, powered by two 3,000 pounds-force (13 kN) Armstrong Siddeley Viper turbojets.
Single engine piston aircraft with tricycle landing gear [1]; Model Engine Power hp Seats Wing Sq. Ft. MTOW lb Empty lb Cruise knots Range nmi AS 202 Bravo NG: L. AEIO-360: 180: 3: 149: 2,202: 1,389
The price for a brand-new private jet ranges from about $2 million to $660 million. The price is determined by many factors, including the size, maker, range, customization and what the jet offers ...
The Dassault Falcon 6X is a large, long-range business jet developed by Dassault Aviation in France. Its precursor, the Falcon 5X twinjet, was launched in 2013, rolled-out in 2015 and made its first flight on July 5, 2017, but its development was frozen as its Safran Silvercrest engine failed to meet performance objectives.
Lufthansa Technik has designed an ultra-luxury cabin for the private jet version of Boeing’s 777X aircraft. ... The long-awaited 777X, the world’s largest twin-engine jet, is expected to enter ...
The Cirrus Vision SF50, also known as the Vision Jet, is a single-engine very light jet designed and produced by Cirrus Aircraft of Duluth, Minnesota, United States. After receiving deposits starting in 2006, Cirrus unveiled an aircraft mock-up on 28 June 2007 and a prototype on 26 June 2008.
The Gulfstream II is a twin-jet swept wing corporate transport powered by two Rolls-Royce Spey turbofan engines and designed to provide high speed and long range capability without sacrificing the airport performance, reliability, and other operational advantages of its predecessor, the turboprop Gulfstream I. Preliminary design of the wing was ...